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1784 lines
100 KiB
Plaintext
Msg#:13387 *AVIATION*
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12/15/91 22:11:31 (Read 0 Times)
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From: IVAN BAIRD
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To: ALL (BLACKBIRD FANS)
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Subj: OXCART
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Blackbird Fans,
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I am at least one person who is extremely intrested in Aviation (especially
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'Black Stuff') and who gets his information, not only from this echo, a mailing
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list on the Internet called Skunk-Works. Recently there has been a lot of
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interest generated by a recently declassified document on the Oxcart Project.
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I thought this might also be of interest here, and so I am writing this note.
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Here is part of the preamble to the actual document, to give you some idea of
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what is in it:
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"This document only talks about OXCART, or what evolved into the A-12 Blackbird
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program. The M-12/D-21 programs and the SR-71 programs are not talked about in
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this document at all, except in cases where to keep OXCART secret, they blamed
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certain A-12 incidents (ex: crashes) on SR-71s."
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This is a fairly large document (about 26-27 pages), and about 95k saved in a
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text only format. This seems a little large to generally release on the echo,
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so I am reluctant to do so. If anybody has any good ideas (I will talk to my
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Boss Node and see if it can be made Freq'able) to get this to the people who
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are interested, without using all the extra $$$ involved for those not
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intrested, please let me know. Also, let me know if your intrested in getting
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this info, I'll compile a list and attempt to make sure everyboby intrested
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gets a copy!
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* Origin: Sea King Surgeon (1:255/3.300)
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Msg#:14427 *AVIATION*
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12/17/91 21:56:00 (Read 0 Times)
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From: DEAN ADAMS
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To: ALL
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Subj: OXCART HISTORY...
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Here is the first part of a 25 page document written by the CIA, about the
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development of the A-12 Blackbird and it's early operational history.
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If enough people are interested, I can keep posting it...
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-----------------------------------------------------------
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Each paragraph is prefixed with the abbreviation of the highest level
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of classified information contained. These are identified by:
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(U) unclassified (S) secret
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(C) confidential (T) top secret
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Oxcart -- Record of a pioneering achievement
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Document downgraded to < Unclassified > 25 Feb 91
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IAW Senior Crown Security Class Guide, dated 11/01/89
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-------------------------------------------------------
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(S) THE OXCART STORY
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Thomas P. McIninch
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(S) One spring day in 1962 a test pilot named Louis Schalk, employed by the
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Lockheed Aircraft Corporation, took off from the Nevada desert in an aircraft
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the like of which had never been seen before. A casual observer would have
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been startled by the appearance of this vehicle; he would perhaps have noticed
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especially its extremely long, slim, shape, its two enormous jet engines, its
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long sharp, projecting nose, and its swept-back wings which appeared far too
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short to support the fuselage in flight. He might well have realized that this
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was a revolutionary airplane; he could not have known that it would be able to
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fly at three times the speed of sound for more than 3,000 miles without
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refueling, or that toward the end of its flight, when fuel began to run low,
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it could cruise at over 90,000 feet. Still less would he have known of the
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equipment it was to carry, or of the formidable problems attending its design
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and construction.
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(U) There was, of course, no casual observer present. The aircraft had been
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designed and built for reconnaissance; it was projected as a successor to the
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U-2. Its development had been carried out in profound secrecy. Despite the
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numerous designers, engineers, skilled and unskilled workers, administrators
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and others who had been involved in the affair, no authentic accounts, and
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indeed scarcely any accounts at all, had leaked. Many aspects have not been
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revealed to this day, and many are likely to remain classified for some time
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to come.
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(S) The official designation of the aircraft was A-12. By a sort of inspired
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perversity, however, it came to be called OXCART, a code word also applied
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to the program under which it was developed. The secrecy in which it was so
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long shrouded has lifted a bit, and the purpose of this article is to give
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someaccount of the inception, development, operation, and untimely demise of
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this remarkable airplane. The OXCART no longer flies, but it left a legacy of
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technological achievement which points the way to new projects. And it became
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the progenitor of a similar but somewhat less sophisticated reconnaissance
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vehicle called the SR-71, whose existence is well known to press and public.
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(S) Sequel to the U-2
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(S) The U-2 dated from 1954, when its development began under the
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direction of a group headed by Richard M. Bissell of CIA. In June 1956, the
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aircraft became operational, but officials predicted that its useful lifetime
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over the USSR could hardly be much more than 18 months or two years. Its first
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flight over Soviet territory revealed that the defense warning system not only
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detected but tracked it quite accurately. Yet, it remained a unique and
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invaluable source of intelligence information for almost four years, until
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on 1 May 1960, Francis Gary Powers was shot down near Sverdlovsk.
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(U) Meanwhile, even as the U-2 commenced its active carreer, efforts were
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under way to make it less vulnerable. The hope was to reduce the vehicle's
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radar cross-section, so that it would become less susceptible to detection.
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New developments in radar-absorbing materials were tried out and achieved
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considerable success, though not enough to solve the problem. Various far-out
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designs were explored, most of them seeking to create an aircraft capable of
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flying at extremely high altitudes, though still at relatively slow speed.
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None of them proved practicable.
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Msg#:14428 *AVIATION*
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12/17/91 21:55:00 (Read 0 Times)
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From: DEAN ADAMS
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To: ALL
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Subj: MORE OXCART
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(S) Eventually, in the fall of 1957, Bissell arranged with a contractor for a
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job of operations analysis to determine how far the probability of shooting
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down an airplane varied respectively with the plane's speed, altitude, and
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radar cross-section. This analysis demonstrated that supersonic speed greatly
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reduced the chances of detection by radar. The probability of being shot down
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was not of course reduced to zero, but it was evident that the supersonic line
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of approach was worth serious consideration. Therefore, from this time on,
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attention focused increasingly on the possibility of building a vehicle which
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could fly at extremely high speeds as well as great altitudes, and which
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would also incorporate the best that could be attained in radar-absorbing
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capabilities. Lockheed Aircraft Corporation and Convair Division of General
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Dynamics were informed of the general requirements, and their designers set
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to work on the problem without as yet receiving any contract or funds from
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the government. From the fall of 1957 to late 1958 these designers constantly
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refined and adapted their respective schemes.
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(S) Bissell realized that development and production of such an aircraft
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would be exceedingly expensive, and that in the early stages at least it would
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be doubtful whether the project could succeed. To secure the necessary funds
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for such a program, high officials would have to receive the best and most
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authoritative presentation of whatever prospects might unfold. Accordingly,
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he got together a panel consisting of two distinguished authorities on aero-
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dynamics and one physicist, with E. M. Land of the Polaroid Corporation as
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chairman. Between 1957 and 1959 this panel met about six times, usually in
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Land's office in Cambridge. Lockheed and Convair designers attended during
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parts of the sessions. So also did the Assistant Secretaries of the Air Force
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and Navy concerned with research and development, together with one or two of
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their technical advisors. One useful consequence of the participation of
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service representatives was that bureaucratic and jurisdictional feuds were
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reduced virtually to nil. Throughout the program both Air Force and Navy gave
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valuable assistance and cooperation.
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(S) As the months went by, the general outlines of what might be done took
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shape in the minds of those concerned. Late in November 1958, the members
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of the panel held a crucial meeting. They agreed that it now appeared feasible
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to build an aircraft of such speed and altitude as to be very difficult to
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track by radar. They recommended that the president be asked to approve in
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principle a further prosecution of the project, and to make funds available
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for further studies and tests. The president and his Scientific Advisor,
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Dr. James Killian were already aware of what was going on, and when CIA
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officials went to them with the recommendations of the panel they received a
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favorable hearing. The President gave his approval. Lockheed and Convair were
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then asked to submit definite proposals, funds were made available to them,
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and the project took on the code name GUSTO.
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(C) Less than a year later the two proposals were essentially complete, and
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on 20 July 1959, the President was again briefed. This time he gave final
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approval, which signified that the program could get fully under way.
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(C) The next major step was to choose between the Lockheed and Convair
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designs. On 20 August 1959 specifications of the two proposals were submitted
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to a joint DOD/USAF/CIA selection panel:
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LOCKHEED CONVAIR
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Speed Mach 3.2 Mach 3.2
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Range (total) 4,120 n.m. 4,000 n.m.
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Range (at altitude) 3,800 n.m. 3,400 n.m.
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Cruise Altitudes:
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Start 84,500 ft. 85,000 ft.
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Mid-range 91,000 ft. 88,000 ft.
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End 97,600 ft. 94,000 ft.
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Dimensions:
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Length 102 ft. 79.5 ft.
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Span 57 ft. 56.0 ft.
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Gross Weight 110,000 lbs. 101,700 lbs.
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Fuel Weight 64,600 lbs. 62,000 lbs.
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First Flight 22 months 22 months
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Msg#:15642 *AVIATION*
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12/20/91 09:46:00 (Read 0 Times)
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From: FRANK WALTERS
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To: DEAN ADAMS
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Subj: REPLY TO MSG# 14427 (RE: OXCART HISTORY...)
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DA> Here is the first part of a 25 page document written by the CIA...
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" (U) unclassified (S) secret
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(C) classified (T) top secret"
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Already I found an error. "(C)" stands for Confidential, not "classified".
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There is no such security category as "classified". It refers to one or all of
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the security classifications. I know you didn't write it, Dean, I just wanted
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to give you an accuracy perspective. If the writer can't get the classification
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categories correct, how many other errors does it contain? Take it with a grain
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of salt. It may be largely true. On the other hand, it could be total B.S.
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(especially if it was "written by the CIA").
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Msg#:15769 *AVIATION*
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12/20/91 02:29:00 (Read 0 Times)
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From: DEAN ADAMS
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To: ALL
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Subj: MORE OXCART...
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[ MORE of the declassified OXCART history ]
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(S) The Lockheed design was selected, Project GUSTO terminated, and the
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program to develop a new U-2 follow-on aircraft was names OXCART. On 3
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September 1959, CIA authorized Lockheed to proceed with antiradar studies,
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aerodynamic structural tests, and engineering designs, and on 30 January 1960
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gave the green light to produce 12 aircraft.
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(S) Pratt and Whitney Division of United Aircraft Corporation had been
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involved in discussions of the project, and undertook to develop the
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propulsion system. Their J-58 engine, which was to be used in the A-12,
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had been sponsored originally by the US Navy for its own purposes, and
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was to be capable of a speed of Mach 3.0. Navy interest in the development
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was diminishing, however, and the Secretary of Defense had decided to withdraw
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from the program at the end of 1959. CIA's requirement was that the engine
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and aircraft be further developed and optimized for a speed of Mach 3.2.
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The new contract called for initial assembly of three advanced experimental
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engines for durability and reliability testing, and provision of three
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engines for experimental flight testing in early 1961.
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(S) The primary camera manufacturer was Perkin-Elmer. Because of the
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extreme complexity of the design, however, a decision was soon made that a
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back-up system might be necessary in the event the Perkin-Elmer design ran
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into production problems, and Eastman Kodak was also asked to build a
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camera. Minneapolis-Honeywell Corporation was selected to provide both the
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(S)inertial navigation and automatic flight control system. The Firewell
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Corporation and the David Clark Corporation became the prime sources of
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pilot equipment and associated life support hardware.
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(U) Lockheed's designer was Clarence L. (Kelly) Johnson, creator of the U-2,
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and he called his new vehicle not A-12 but A-11. Its design exhibited many
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innovations. Supersonic airplanes, however, involve a multitude of extremely
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difficult design problems. Their payload-range performance is highly sensitive
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to engine weight, structural weight, fuel consumption, and aerodynamic
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efficiency. Small mistakes in predicting these values can lead to large
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errors in performance. Models of the A-11 were tested and retested, adjusted
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and readjusted, during thousands of hours in the wind tunnel. Johnson was
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confident of his design, but no one could say positively whether the bird
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would fly, still less whether it would fulfill the extremely demanding
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requirements laid down for it.
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(U) To make the drawings and test the model was one thing; to build the air-
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craft was another. The most numerous problems arose from the simple fact
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that in flying through the atmosphere at its designed speed the skin of the
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air-craft would be subjected to a temperature of more than 550 degrees
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Fahrenheit. For one thing, no metal hitherto commonly used in aircraft
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production would stand this temperature, and those which would do so were
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for the most part too heavy to be suitable for the purpose in hand.
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(S) During the design phase Lockheed evaluated many materials and finally
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chose an alloy of titanium, characterized by great strength, relatively light
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weight, and good resistance to high temperatures. Titanium was also scarce
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and very costly. Methods for milling it and controlling the quality of the
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product were not fully developed. Of the early deliveries from Titanium
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Metals Corporation some 80 percent had to be rejected, and it was not until
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1961, when a delegation from headquarters visited the officials of that
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company, informed them of the objectives and high priority of the OXCART
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program, and gained their full cooperation, that the supply became consist-
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ently satisfactory.
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(S) But this only solved an initial problem. One of the virtues of titanium
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was its exceeding hardness, but this very virtue gave rise to immense
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difficulties in machining and shaping the material. Drills which worked well
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on aluminum soon broke to pieces; new ones had to be devised. Assembly-line
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production was impossible; each of the small OXCART fleet was, so to speak,
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turned out by hand. The cost of the program mounted well above original
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estimates, and it soon began to run behind schedule. One after another,
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however, the problems were solved, and their solution constituted the greatest
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single technological achievement of the entire enterprise. Henceforth it
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became practicable, if expensive, to build aircraft out of titanium.
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Msg#:16306 *AVIATION*
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12/20/91 21:44:00 (Read 0 Times)
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From: DEAN ADAMS
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To: ALL
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Subj: MORE OXCART
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[ here is the 4th installment of this declassified OXCART history ]
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(S) Since every additional pound of weight was critical, adequate insulation
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was out of the question. The inside of the aircraft would be like a moderately
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hot oven. The pilot would have to wear a kind of space suit, with its own
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cooling apparatus, pressure control, oxygen supply, and other necessities for
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survival. The fuel tanks, which constituted by far the greater part of the
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aircraft, would heat up to about 350 degrees, so that special fuel had to be
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supplied and the tanks themselves rendered inert with nitrogen. Lubricating
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oil was formulated for operation at 600 degrees F., and contained a diluent in
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order to remain fluid at operation below 40 degrees. Insulation on the plane's
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intricate wiring soon became brittle and useless. During the lifetime of the
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OXCART no better insulation was found; the wiring and related connectors had
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to be given special attention and handling at great cost in labor and time.
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(S) Then there was the unique problem of the camera window. The OXCART was
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to carry a delicate and highly sophisticated camera, which would look out
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through a quartz glass window. The effectiveness of the whole system depended
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upon achieving complete freedom from optical distortion despite the great
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heat to which the window would be subjected. Thus the question was not simply
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one of providing equipment with resistance to high temperature, but of
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assuring that there should be no unevenness of temperature throughout the
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area of the window. It took three years of time and two million dollars of
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money to arrive at a satisfactory solution. The program scored one of its
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most remarkable successes when the quartz glass was successfully fused to
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its metal frame by an unprecedented process involving the use of high
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frequency sound waves.
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(S) Another major problem of different nature was to achieve the low radar
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cross-section desired. The airframe areas giving the greatest radar return
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were the vertical stabilizers, the engine inlet, and the forward side of the
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engine nacelles. Research in ferrites, high temperature absorbing materials
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and high-temperature plastic structures was undertaken to find methods to
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reduce the return. Eventually the vertical tail section fins were constructed
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from a kind of laminated "plastic" material-the first time that such a
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material had been used for an important part of an aircraft's structure.
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With such changes in structural materials, the A-11 was redesignated A-12,
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and as such has never been publically disclosed.
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(C) To test the effectiveness of antiradar devices a small-scale model is
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inadequate; only a full-size mock-up will do. Lockheed accordingly built one
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of these, and as early as November 1959, transported it in a specially
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designed trailer truck over hundreds of miles of highway from the Burbank
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plant to the test area. Here it was hoisted to the top of a pylon and looked
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at from various angles by radar. Tests and adjustments went on for a year and
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a half before the results were deemed satisfactory. In the course of the
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process it was found desirable to attach some sizable metallic constructions
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on each side of the fuselage, and Kelly Johnson worried a good deal about the
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effect of these protuberances on his design. In flight tests, however, it
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later developed that they imparted a useful aerodynamic lift to the vehicle,
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and years afterward Lockheed's design for a supersonic transport embodied
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similar structures.
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(S) Pilots for the OXCART would obviously have to be of quite extraordinary
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competence, not only because of the unprecedented performance of the aircraft
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itself, but also because of the particluar qualities needed in men who were
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to fly intelligence missions. Brigadier General Don Flickinger, of the Air
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||
Force, was designated to draw up the criteria for selection, with advice from
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Kelly Johnson and from CIA Headquarters. Pilots had to be qualified in the
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latest high performance fighters, emotionally stable, and well motivated.
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They were to be between 25 and 40 years of age, and the size of the A-12
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cockpit prescribed that they be under six feet tall and under 175 pounds
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in weight.
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Msg#:16307 *AVIATION*
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12/20/91 21:50:00 (Read 0 Times)
|
||
From: DEAN ADAMS
|
||
To: ALL
|
||
Subj: MORE OXCART
|
||
[ here is the 5th installment of this declassified OXCART history ]
|
||
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(S) Air Force files were screened for possible candidates and a list of pilots
|
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obtained. Psychological assessments, physical examinations and refinement of
|
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criteria eliminated a good many. Pre-evaluation processing resulted in sixteen
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||
potential nominees. This group underwent a further intensive security and
|
||
medical scrutiny by the Agency. Those who remained were then approached to
|
||
take employment with the Agency on a highly classified project involving a
|
||
very advanced aircraft. In November 1961, commitments were obtained from
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||
five of the group. The small number recruited at this stage required that a
|
||
second search be undertaken.
|
||
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(S) When the final screening was complete the pilots selected from the
|
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program were William L. Skliar, Kenneth S. Collins, Walter Ray, Lon Walter,
|
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Mele Vojvodich, Jr., Jack W. Weeks, Ronald "Jack" Layton, Dennis B. Sullivan,
|
||
David P. Young, Francis J. Murray, and Russell Scott. After the selection,
|
||
arrangements were made with the Air Force to effect appropriate transfers
|
||
and assignments to cover their training and to lay the basis for their
|
||
transition from military to civilian status. Compensation and insurance
|
||
arrangements were similar to those for the U-2 pilots.
|
||
|
||
(U) One thing to be decided in the earliest stages of the program was where
|
||
to base and test the aircraft. Lockheed clearly could not do the business at
|
||
Burbank, where the aircraft were being built, if for no other reason that its
|
||
runway was too short. The ideal location ought to be remote from metropolitan
|
||
areas; well away from civil and military airways to preclude observation;
|
||
easily accessible by air; blessed with good weather the year round; capable
|
||
of accommodating large numbers of personnel; equipped with fuel storage
|
||
facilities; fairly close to an Air Force installation; and possessing at
|
||
least an 8,000 foot runway. There was no such place to be found.
|
||
|
||
(S) Ten Air Force bases programmed for closure were considered, but none
|
||
provided the necessary security, and annual operating costs at most of them
|
||
would be unacceptable. Edwards Air Force Base in California seemed a more
|
||
likely candidate, but in the end it also was passed over. Instead a secluded
|
||
site in Nevada was finally picked. It was deficient in personnel accomodations
|
||
and POL storage, and its long-unused runway was inadequate, but security was
|
||
good, or could be made so, and a moderate construction program could provide
|
||
sufficient facilities. Lockheed estimated what would be needed in such
|
||
respects as monthly fuel consumption, hangars and shop space, housing for
|
||
personnel, and runway specifications. Armed with the list of major
|
||
requirements, Headquarters came up with a construction and engineering plan.
|
||
And in case anyone became curious about what was going on at this remote
|
||
spot, a cover story stated that the facilities were being prepared for
|
||
certain radar studies, to be conducted by an engineering firm with support
|
||
from the Air Force. The remote location was explained as necessary to reduce
|
||
the effect of electronic interference from outside sources.
|
||
|
||
(S) Excellent as it may have been from the point of view of security, the site
|
||
at first afforded few of the necessities and none of the amenities of life.
|
||
It was far from any metropolitan center. Lockheed provided a C-47 shuttle
|
||
service to its plant at Burbank, and a chartered D-18 (Lodestar) furnished
|
||
transportation to Las Vegas. Daily commuting was out of the question, however,
|
||
and the construction workers arriving during 1960 were billeted in surplus
|
||
trailers. A new water well was dug, and a few recreational facilities
|
||
provided, but it was some time before accomodations became agreeable.
|
||
|
||
Msg#:16308 *AVIATION*
|
||
12/20/91 21:54:00 (Read 0 Times)
|
||
From: DEAN ADAMS
|
||
To: ALL
|
||
Subj: MORE OXCART
|
||
[ here is the 6th installment of this declassified OXCART history ]
|
||
|
||
(S) Among the lesser snags, one existed because the laws of Nevada required
|
||
the names of all contractor personnel staying in the state for more than 48
|
||
hours to be reported to state authorities. It was generally felt that to list
|
||
all these names and identify the companies involved would be likely to give
|
||
the whole show away. The Agency's General Counsel, however, discovered that
|
||
Government employees were exempted from these requirements. Thence forth
|
||
all contractor personnel going to the site received appointments as Government
|
||
consultants, and if questions were asked the reply could be that no one but
|
||
government employees were at this site.
|
||
|
||
(C) Construction began in earnest in September 1960, and continued on a
|
||
double-shift schedule until mid-1964. One of the most urgent tasks was to
|
||
build the runway, which according to initial estimates of A-12 requirements
|
||
must be 8,500 feet long. The existing asphalt runway was 5,000 feet long and
|
||
incapable of supporting the weight of the A-12. The new one was built between
|
||
7 September and 15 November and involved pouring over 25,000 yards of
|
||
concrete. Another major problem was to provide some 500,000 gallons of PF-1
|
||
aircraft fuel per month. Neither storage facilities nor means of transporting
|
||
fuel existed. After considering airlift, pipeline, and truck transport, it
|
||
was decided that the last-named was the most economical, and could be made
|
||
feasible by resurfacing no more than eighteen miles of highway leading into
|
||
the base.
|
||
|
||
(C) Three surplus Navy hangars were obtained, dismantled, and erected on
|
||
the north side of the base. Over 100 surplus Navy housing buildings were
|
||
transported to the base and made ready for occupancy. By early 1962 a fuel
|
||
tank farm was ready, with a capacity of 1,320,000 gallons. Warehousing and
|
||
shop space was begun and repairs made to older buildings. All this, together
|
||
with the many other facilities that had to be provided, took a long time to
|
||
complete. Meanwhile, however, the really essential facilities were ready in
|
||
time for the forecast delivery date of Aircraft No. 1 in August 1961.
|
||
|
||
(S) The facilities were ready, but the aircraft were not. Originally promised
|
||
for delivery at the end of May 1961, the date first slipped to August, largely
|
||
because of Lockheed's difficulties in procuring and fabricating titanium.
|
||
Moreover, Pratt & Whitney found unexpectedly great trouble in bringing the
|
||
J-58 engine up to OXCART requirements. In March 1961, Kelly Johnson
|
||
notified Headquarters:
|
||
|
||
(U) "Schedules are in jeopardy on two fronts. One is the assembly of the
|
||
wing and the other is in satisfactory development of the engine.
|
||
Our evaluation shows that each of these programs is from three to
|
||
four months behind the current schedule."
|
||
|
||
(S) To this Bissell replied:
|
||
|
||
(U) "I have learned of your expected additional delay in first flight
|
||
from 30 August to 1 December 1961. This news is extremely shocking
|
||
on top of our previous slippage from May to August and my understanding
|
||
as of our meeting 19 December that the titanium extrusion problems
|
||
were essentially overcome. I trust this is the last of such
|
||
disappointments short of a severe earthquake in Burbank."
|
||
|
||
(U) Realizing that delays were causing the cost of the program to soar,
|
||
Headquarters decided to place a top-level aeronautical engineer in residence
|
||
at Lockheed to monitor the program and submit progress reports.
|
||
|
||
Msg#:16310 *AVIATION*
|
||
12/21/91 04:37:00 (Read 0 Times)
|
||
From: DEAN ADAMS
|
||
To: ALL
|
||
Subj: MORE OXCART
|
||
[ here is the 7th installment of this declassified OXCART history ]
|
||
|
||
(C) Delays nevertheless persisted. On 11 September, Pratt and Whitney
|
||
informed Lockheed of their continuing difficulties with the J-58 engine in
|
||
terms of weight, delivery, and performance. Completion date for Aircraft
|
||
No. 1 by now had slipped to 22 December 1961, and the first flight to 27
|
||
February 1962. Even on this last date the J-58 would not be ready, and it was
|
||
therefore decided that a Pratt and Whitney J-75 engine, designed for the F-105
|
||
and flown in the U-2, should be used for early flights. The engine, along with
|
||
other components, could be fitted to the A-12 airframe, and it could power the
|
||
aircraft safely to altitudes up to 50,000 feet and at speeds up to Mach 1.6.
|
||
|
||
(S) When this decision had been made, final preparations were begun for the
|
||
testing phase. In late 1961 Colonel Robert J. Holbury, USAF, was named
|
||
Commander of the base, with the Agency employee as his Deputy. Support
|
||
aircraft began arriving in the spring of 1962. These included eight F-101's
|
||
for training, two T-33's for proficiency flying, a C-130 for cargo transport,
|
||
a U-3A for administration purposes, a helicopter for search and rescue, and a
|
||
Cessna-180 for liaison use. In addition, Lockheed provided an F-104 to act as
|
||
chase aircraft during the A-12 flight test period.
|
||
|
||
(S) Meanwhile in January 1962, an agreement was reached with the Federal
|
||
Aviation Agency that expanded the restricted airspace in the vicinity of the
|
||
test area. Certain FAA air traffic controllers were cleared for the OXCART
|
||
Project; their function was to insure that aircraft did not violate the order.
|
||
The North American Air Defense Command established procedures to prevent
|
||
their radar stations from reporting the appearance of high performance
|
||
aircraft on their radar scopes.
|
||
|
||
(S) Refueling concepts required prepositioning of vast quantities of fuel at
|
||
certain points outside the United States. Special tank farms were programmed
|
||
in California, Eielson AFB Alaska, Thule AB Greenland, Kadena AB Okinawa,
|
||
and Adana, Turkey. Since the A-12 use specially refined fuel, these tank
|
||
farms were reserved exclusively for use by the OXCART Program. Very small
|
||
detachments of technicians at these locations maintained the fuel storage
|
||
facility and arranged for periodic quality control fuel tests.
|
||
|
||
(S) At the Lockheed Burbank plant, Aircraft No. 1 (serially numbered 121)
|
||
received its final tests and checkout during January and February 1962, and
|
||
was partially disassembled for shipment to the site. It became clear very
|
||
early in OXCART planning that because of security problems and the inadequate
|
||
runway, the A-12 could not fly from Burbank. Movement of the full-scale
|
||
radar test model had been successfully accomplished in November 1959, as
|
||
described above. A thorough survey of the route in June 1961, ascertained
|
||
the hazards and problems of moving the actual aircraft, and showed that a
|
||
package measuring 35 feet wide and 105 feet long could be transported
|
||
without major difficulty. Obstructing road signs had to be removed, trees
|
||
trimmed, and some roadsides leveled. Appropriate arrangements were made
|
||
with police authorities and local officials to accomplish the safe transport
|
||
of the aircraft. The entire fuselage, minus wings, was crated, covered, and
|
||
loaded on the special-design trailer, which cost about $100,000. On 26
|
||
February 1962, it departed Burbank, and arrived at the base according to plan.
|
||
|
||
(S) First Flights
|
||
|
||
(U) Upon arrival reassembly of the aircraft and installation of the J-75
|
||
engines began. Soon it was found that aircraft tank sealing compounds had
|
||
failed to adhere to the metals, and when fuel was put into the tanks numerous
|
||
leaks occurred. It was necessary to strip the tanks of the faulty sealing
|
||
compounds and reline them with new materials. Thus occurred one more
|
||
unexpected and exasperating delay in the program.
|
||
|
||
Msg#:16311 *AVIATION*
|
||
12/21/91 04:42:00 (Read 0 Times)
|
||
From: DEAN ADAMS
|
||
To: ALL
|
||
Subj: MORE OXCART
|
||
[ here is the 8th installment of this declassified OXCART history ]
|
||
|
||
(U) Finally, on 26 April 1962, Aircraft 121 was ready. On that day in
|
||
accordance with Kelly Johnson's custom, Louis Schalk took it for an
|
||
unofficial, unannounced, maiden flight lasting some 40 minutes. As in all
|
||
maiden flights minor problems were detected, but it took only four more
|
||
days to ready the aircraft for its first official flight.
|
||
|
||
(U) On 30 April 1962, just under one year later than originally planned, the
|
||
A-12 officially lifted her wheels from the runway. Piloted again by Louis
|
||
Schalk, it took off at 170 knots, with a gross weight of 72,000 pounds, and
|
||
climbed to 30,000 feet. Top speed was 340 knots and the flight lasted 59
|
||
minutes. The pilot reported that the aircraft responded well and was
|
||
extremely stable. Kelly Johnson declared it to be the smoothest official first
|
||
flight of any aircraft he had designed or tested. The aircraft broke the sound
|
||
barrier on its second official flight, 4 May 1962, reaching Mach 1.1. Again
|
||
only minor problems were reported.
|
||
|
||
(S) With these flights accomplished, jubilation was the order of the day. The
|
||
new Director of Central Intelligence, Mr. John McCone, sent a telegram of
|
||
congratulation to Kelly Johnson. A critical phase had been triumphantly
|
||
passed, but there remained the long, difficult, and sometimes discouraging
|
||
process of working the aircraft up to full operational performance.
|
||
|
||
(C) Aircraft No. 122 arrived at base on 26 June, and spent three months in
|
||
radar testing before engine installations and final assembly. Aircraft No. 123
|
||
arrived in August and flew in October. Aircraft No. 124, a two-seated version
|
||
intended for use in training project pilots, was delivered in November. It was
|
||
to be powered by the J-58 engines, but delivery delays and a desire to begin
|
||
pilot training prompted a decision to install the smaller J-75's. The trainer
|
||
flew initially in January 1963. The fifth aircraft, No. 125, arrived at the
|
||
area on 17 December.
|
||
|
||
(S) Meanwhile the OXCART program received a shot in the arm from the Cuban
|
||
missile crisis. U-2's had been maintaining a regular reconnaissance vigil
|
||
over the island, and it was on one of these missions in October that the
|
||
presence of offensive missiles was discovered. Overflights thereafter became
|
||
more frequent, but on 27 October an Agency U-2, flown by a Strategic Air
|
||
Force pilot on a SAC-directed mission, was shot down by a surface-to-air
|
||
missile. This raised the dismaying possibility that continued manned, high-
|
||
altitude surveillance of Cuba might become out of the question. The OXCART
|
||
program suddenly assumed greater significance than ever, and its achievement
|
||
of operational status became one of the highest national priorities.
|
||
|
||
(S) At the end of 1962 there were two A-12 aircraft engaged in flight tests.
|
||
A speed of Mach 2.16 and altitude of 60,000 feet had been achieved. Progress
|
||
was still slow, however, because of delays in the delivery of engines and
|
||
shortcomings in the performance of those delivered. One of the two test
|
||
aircraft was still flying with two J-75 engines, and the other with one J-75
|
||
and one J-58. It had long since become clear that Pratt & Whitney had been
|
||
too optimistic in their forecast; the problem of developing the J-58 up to
|
||
OXCART specifications had proved a good deal more recalcitrant than expected.
|
||
Mr. McCone judged the situation to be truly serious, and on 3 December he wrote
|
||
to the President of United Aircraft Corporation.
|
||
|
||
(U) "I have been advised that J-58 engine deliveries have been delayed
|
||
again due to engine control production problems....By the end of
|
||
the year it appears we will have barely enough J-58 engines to
|
||
support the flight test program adequately....Furthernore, due to
|
||
various engine difficulties we have not yet reached design speed and
|
||
altitude. Engine thrust and fuel consumption deficiencies at pres-
|
||
ent prevent sustained flight at design conditions which is so
|
||
necessary to complete developments."
|
||
|
||
(U) By the end of January 1963, ten engines were available, and the first
|
||
flight with two of them installed occurred on 15 January. Thenceforth all
|
||
A-12 aircraft were fitted with their intended propulsion system. Flight
|
||
testing accelerated and contractor personnel went to a three-shift work day.
|
||
|
||
Msg#:17119 *AVIATION*
|
||
12/21/91 21:58:00 (Read 0 Times)
|
||
From: DEAN ADAMS
|
||
To: FRANK WALTERS
|
||
Subj: RE: OXCART HISTORY...
|
||
DA>> Here is the first part of a 25 page document written by the CIA...
|
||
FW> (C) classified (T) top secret"
|
||
|
||
FW> "(C)" stands for Confidential, not "classified".
|
||
|
||
Yes, you are correct. I should have noticed that when I stuck that
|
||
note into the beginning of the file...
|
||
|
||
FW> I know you didn't write it, Dean, I just wanted to give you an
|
||
FW> accuracy perspective. If the writer can't get the classification
|
||
FW> categories correct, how many other errors does it contain?
|
||
|
||
Rest assured! THAT "definition" listing was *NOT* in the original document.
|
||
I picked it up during some early discussions about this, and added it to the
|
||
beginning of the text. EVERYTHING -after- that part is a verbatim transcript
|
||
of the original document. When this was first coming out, someone else with
|
||
experience in classifications already made the same correction you did, almost
|
||
word for word, but I must have only saved the original version of that note
|
||
and forgot to change it.
|
||
|
||
FW> Take it with a grain of salt. It may be largely true. On the other
|
||
FW> hand, it could be total B.S.
|
||
|
||
NO. It has been "verified" by SEVERAL people in official capacities.
|
||
Including some from the 9th SRW, and others such as someone from NASA who
|
||
obtained a copy of it from their own sources, and who has the same "Senior
|
||
Crown" security clearance this document was originally classified under...
|
||
|
||
FW> especially if it was "written by the CIA".
|
||
|
||
That was also verified by some people who should know. The document was
|
||
described as a "CIA history", and the man who wrote it Thomas P. McIninch
|
||
is/was an author for the CIA. There have already been quotes from this same
|
||
document appearing in Aviation Week. It is very definitely "real"...
|
||
|
||
BTW, here are a few more items of detail from the cover page:
|
||
|
||
CLASSIFIED BY: SR CROWN SECURITY
|
||
CLASSIFICATION ?U? , 25 MAY 87
|
||
DECLASSIFY ??: ??? 3
|
||
|
||
DON: < SC-86-010115 >
|
||
COPY NO. < ?01 >
|
||
TOTAL PAGES < 25 >
|
||
|
||
On the front and back covers, the document is marked with the highest security
|
||
classification contained within the entire document. Each page is also marked
|
||
with the highest level contained on the page.
|
||
|
||
Msg#:17129 *AVIATION*
|
||
12/21/91 20:20:00 (Read 0 Times)
|
||
From: DEAN ADAMS
|
||
To: ALL
|
||
Subj: MORE OXCART
|
||
[ here is the 9th installment of this declassified OXCART history ]
|
||
|
||
(U) With each succeeding step into a high Mach regime new problems presented
|
||
themselves. The worst of all these difficulties-indeed one of the most
|
||
formidable in the entire history of the program-was revealed when flight
|
||
testing moved into speeds between Mach 2.4 and 2.8, and the aircraft
|
||
experienced such severe roughness as to make its operation virtually out of
|
||
the question. The trouble was diagnosed as being in the air inlet system,
|
||
which with its controls admitted air to the engine. At the higher speeds the
|
||
flow of air was uneven, and the engine therefore could not function properly.
|
||
Only after a long period of experimentation, often highly frustrating and
|
||
irritating, was a solution reached. This further postponed the day when the
|
||
A-12 could be declared operationally ready.
|
||
|
||
(U) Among more mundane troubles was the discovery that various nuts, bolts,
|
||
clamps, and other debris of the manufacturing process had not been cleared
|
||
away, and upon engine runup or take-off were sucked into the engine. The
|
||
engine parts were machined to such close tolerances that they could be ruined
|
||
in this fashion. Obviously the fault was due to sheer carelessness. Inspection
|
||
procedures were revised, and it was also found prudent at Burbank to hoist
|
||
the engine nacelles into the air, rock them back and forth, listen for loose
|
||
objects, and then remove them by hand.
|
||
|
||
(S) While on a routine flight, 24 May 1963, one of the detachment pilots rec-
|
||
ognized an erroneous and confusing air speed indication and decided to eject
|
||
from the aircraft, which crashed 14 miles south of Wendover, Utah. The pilot
|
||
Kenneth Collins, was unhurt. The wreckage was recovered in two days, and
|
||
persons at the scene were indentified and requested to sign secrecy agreements.
|
||
A cover story for the press described the accident as occurring to a F-105, and
|
||
is still listed in this way on official records.
|
||
|
||
(U) All A-12 aircraft were grounded for a week during investigation of the
|
||
accident. A plugged pitot static tube in icing conditions turned out to be
|
||
responsible for the faulty cockpit instrument indications-it was not some-
|
||
thing which would hold things up for long.
|
||
|
||
(S) Loss of this aircraft nevertheless precipitated a policy problem which had
|
||
been troubling the Agency for some time. With the growing number of A-12's,
|
||
how much longer could the project remain secret? The program had gone through
|
||
development, construction, and a year of flight testing without attracting
|
||
public attention. But the Department of Defense was having difficulty in
|
||
concealing its participation because of the increasing rate of expenditures,
|
||
otherwise unexplained. There was also a realization that the technological
|
||
data would be extremely valuable in connection with feasibility studies for the
|
||
SST. Finally, there was a growing awareness in the higher reaches of the
|
||
aircraft industry that something new and remarkable was going on. Rumors
|
||
spread, and gossip flew about. Commercial airline crews sighted the OXCART in
|
||
flight. The editor of Aviation Week (as might be expected) indicated his
|
||
knowledge of developments at Burbank. The secrecy was thinning out.
|
||
|
||
(S) The President's Announcement
|
||
|
||
(U) In spite of all this, 1963 went by without any public revelation. President
|
||
Johnson was brought up to date on the project a week after taking office, and
|
||
directed that a paper be prepared for an announcement in the spring of 1964.
|
||
Then at his press conference on 24 February, he read a statement of which the
|
||
first paragraph was as follows:
|
||
|
||
(U) "The United States has successfully developed an advanced experi-
|
||
mental jet aircraft, the A-11, which has been tested in sustained
|
||
flight at more than 2,000 miles per hour and at altitudes in excess
|
||
of 70,000 feet. The performance of the A-11 far exceeds that of any
|
||
other aircraft in the world today. The development of this aircraft
|
||
has been made possible by major advances in aircraft technology of
|
||
great significance for both military and commercial applications.
|
||
Several A-11 aircraft are now being flight tested at Edwards Air
|
||
Force Base in California. The existence of this program is being
|
||
disclosed today to permit the orderly exploitation of this advanced
|
||
technology in our military and commercial program."
|
||
|
||
Msg#:17130 *AVIATION*
|
||
12/21/91 20:28:00 (Read 0 Times)
|
||
From: DEAN ADAMS
|
||
To: ALL
|
||
Subj: MORE OXCART
|
||
[ here is the 10th installment of this declassified OXCART history ]
|
||
|
||
(U) The president went on to mention the "mastery of the metallurgy and
|
||
fabrication of titanium metal" which has been achieved, gave credit to
|
||
Lockheed and to Pratt & Whitney, remarked that appropriate members of the
|
||
Senate and House had been kept fully informed, and prescribed that the
|
||
detailed performance of the A-11 would be kept strictly classified.
|
||
|
||
(S) The President's reference to the "A-11" was of course deliberate. "A-11"
|
||
had been the original design designation for the all-metal aircraft first
|
||
proposed by Lockheed; subsequently it became the design designation for the
|
||
Air Force YF-12A interceptor which differed from its parent mainly in that it
|
||
carried a second man for launching air-to-air missiles. To preserve the
|
||
distinction between the A-11 and the A-12 Security had briefed practically all
|
||
witting personnel in government and industry on the impending announcement.
|
||
OXCART secrecy continued in effect. There was considerable speculation about
|
||
an Agency role in the A-11 development, but it was never acknowledged by the
|
||
government. News headlines ranged from "US has dozen A-11 jets already
|
||
flying" to "Secret of sizzling new plane probably history's best kept."
|
||
|
||
(U) The President also said that "the A-11 aircraft now at Edwards Air Force
|
||
Base are undergoing extensive tests to determine their capabilities as long-
|
||
range interceptors." It was true that the Air Force in October 1960, had
|
||
contracted for three interceptor versions of the A-12, and they were by this
|
||
time available. But at the moment when the President spoke, there were no
|
||
A-11's at Edwards and there never had been. Project officials had known that
|
||
the public announcement was about to be made, but they had not been told
|
||
exactly when. Caught by surprise, they hastily flew two Air Force YF-12A's to
|
||
Edwards to support the President's statement. So rushed was this operation, so
|
||
speedily were the aircraft put into hangars upon arrival, that heat from them
|
||
activated the hangar sprinkler system, dousing the reception team which awaited
|
||
them.
|
||
|
||
(S) Thenceforth, while the OXCART continued its secret career at its own site,
|
||
the A-11 performed at Edwards Air Force Base in a considerable glare of
|
||
publicity. Pictures of the aircraft appeared in the press, correspondents
|
||
could look at it and marvel, stories could be written. Virtually no details
|
||
were made available, but the technical journals nevertheless had a field day.
|
||
The unclassified Air Force and Space Digest, for example, published a long
|
||
article in its issue of April 1964, commencing: "The official pictures and
|
||
statements tell very little about the A-11. But the technical literature from
|
||
open sources, when carefully interpreted, tells a good deal about what it
|
||
could and, more importantly, what it could not be. Here's the story ..."
|
||
|
||
(S) Going Operational
|
||
|
||
(U) Three years and seven months after first flight in April 1962 the OXCART
|
||
was declared ready for operational use at design specifications. The period
|
||
thus devoted to flight tests was remarkably short, considering the new fields
|
||
of aircraft performance which were being explored. As each higher Mach number
|
||
was reached exhaustive tests were carried out in accordance with standard
|
||
procedures to ensure that the aircraft functioned properly and safely.
|
||
Defects were corrected and improvements made. All concerned gained experience
|
||
with the particular characteristics and idiosyncrasies of the vehicle.
|
||
|
||
(S) The air inlet and related control continued for a long time to present the
|
||
most troublesome and refractory problem. Numerous attempts failed to find a
|
||
remedy, even though a special task force concentrated on the task. For a time
|
||
there was something approaching despair, and the solution when finally
|
||
achieved was greeted with enormous relief. After all, not every experimental
|
||
aircraft of advanced performance has survived its flight testing period. The
|
||
possibility existed that OXCART also would fail, despite the great cost and
|
||
effort expended upon it.
|
||
|
||
Message #3394 "Aviation"
|
||
Date: 24-Dec-91 18:47
|
||
From: Dean Adams
|
||
To: Albert Dobyns
|
||
Subj: Re: OXCART PART 11?
|
||
AD> Dean, I was rereading your OXCART files and noticed that part 10 is
|
||
AD> followed by part 12. But no part 11?! Naturally I wouldn't want to
|
||
AD> miss even a single sentence of this stuff so I thought I'd let you know.
|
||
|
||
That one went out with the others. I guess Fido could have eaten it. Here is
|
||
another copy, let's hope no more get lost as well...
|
||
[ the 11th installment of this declassified OXCART history ]
|
||
|
||
(S) A few dates and figures will serve to mark the progress of events. By the
|
||
end of 1963 there had been 573 flights totalling 765 hours. Nine aircraft were
|
||
in the inventory. On 20 July 1963 test aircraft flew for the first time at
|
||
Mach 3; in November Mach 3.2 (the design speed) was reached at 78,000 feet
|
||
altitude. The longest sustained flight at design conditions occurred on 3
|
||
February 1964; it lasted to ten minutes at Mach 3.2 and 83,000 feet. By the
|
||
end of 1964 there had been 1,160 flights, totalling 1,616 hours. Eleven
|
||
aircraft were then available, four of them reserved for testing and seven
|
||
assigned to the detachment.
|
||
|
||
(C) The record may be put in another way. Mach 2 was reached after six months
|
||
of flying; Mach 3 after 15 months. Two years after the first flight the
|
||
aircraft had flown a total of 38 hours at Mach 2, three hours at Mach 2.6, and
|
||
less than one hour at Mach 3. After three years, Mach 2 time had increased to
|
||
60 hours, Mach 2.6 time time to 33 hours, and Mach 3 time to nine hours; all
|
||
Mach 3 time, however, was by test aircraft, and detachment aircraft were still
|
||
restricted to Mach 2.9.
|
||
|
||
(S) As may be seen from the figures, most flights were of short duration,
|
||
averaging little more than an hour each. Primarily this was because longer
|
||
flights were unnecessary at this stage of testing. It was also true, however,
|
||
that the less seen of OXCART the better, and short flights helped to preserve
|
||
the secrecy of the proceedings. Yet it was virtually impossible for an
|
||
aircraft of such dimensions and capabilities to remain inconspicuous. At its
|
||
full speed OXCART had a turning radius of no less than 86 miles. There was no
|
||
question of staying close to the airfield; its shortest possible flights took
|
||
it over a very large expanse of territory.
|
||
|
||
(S) The first long-range, high-speed flight occurred on 27 January 1965, when
|
||
one of the test aircraft flew for an hour and forty minutes, with an hour and
|
||
fifteen minutes above Mach 3.1. Its total range was 2,580 nautical miles, with
|
||
altitudes between 75,600 and 80,000 feet.
|
||
|
||
(U) Two more aircraft were lost during this phase of the program. On 9 July
|
||
1964 Aircraft No. 133 was making its final approach to the runway when at
|
||
altitude of 500 feet and airspeed of 200 knots it began a smooth steady roll
|
||
to the left. Lockheed test pilot Bill Park could not overcome the roll. At
|
||
about a 45 degree bank angle and 200 foot altitude he ejected. As he swung
|
||
down to the vertical in the parachute his feet touched the ground, for what
|
||
must have been one of the narrower escapes in the perilous history of test
|
||
piloting. The primary cause of the accident was that the servo for the right
|
||
outboard roll and pitch control froze. No news of the accident filtered out.
|
||
|
||
(S) On 28 December 1965 Aircraft No. 126 crashed immediately after takeoff and
|
||
was totally destroyed. Detachment pilot Mele Vojvodich ejected safely at an
|
||
altitude of 150 feet. The accident investigation board determined that a
|
||
flight line electrician had improperly connected the yaw and pitch gyros-had
|
||
in effect reversed the controls. This time Mr. McCone directed the Office of
|
||
Security to conduct an investigation into the possibility of sabotage. While
|
||
nothing of the sort was discovered, there were indications of negligence, as
|
||
the manufacturer of the gyro had earlier warned of the possibility that the
|
||
mechanism could be connected in reverse. No action had been taken, however,
|
||
even by such an elementary precaution as painting the contacts different
|
||
colors. Again there was no publicity connected with the accident.
|
||
|
||
(S) The year 1965 saw the test site reach the high point of activity.
|
||
Completion of construction brought it to full physical size. All detachment
|
||
pilots were Mach 3.0 qualified. Site population reached 1,835. Contractors
|
||
were working three shifts a day. Lockheed Constellations made daily flights
|
||
between the factory at Burbank and the site. Two C-47 flights a day were
|
||
made between the site and Las Vegas. And officials were considering how and
|
||
when and where to use OXCART in its appointed role.
|
||
|
||
Msg#:17131 *AVIATION*
|
||
12/21/91 20:31:00 (Read 0 Times)
|
||
From: DEAN ADAMS
|
||
To: ALL
|
||
Subj: MORE OXCART
|
||
[ here is the 12th installment of this declassified OXCART history ]
|
||
|
||
(S) Targeting the OX
|
||
|
||
(S) After the unhappy end of U-2 flights over the Soviet Union, US political
|
||
authorities were understandably cautious about committing themselves to
|
||
further manned reconnaissance over unfriendly territory. There was no serious
|
||
intention to use the OXCART over Russia; save in some unforseeable emergency it
|
||
was indeed no longer necessary to do so. What then, should be done with this
|
||
vehicle?
|
||
|
||
(S) The first interest was in Cuba. By early 1964 Project Headquarters began
|
||
planning for the contingency of flights over that island under a program
|
||
designated SKYLARK. Bill Park's accident in early July held this program up
|
||
for a time, but on 5 August Acting DCI Marshall S. Carter directed that
|
||
SKYLARK achieve emergency operational readiness by 5 November. This involved
|
||
preparing a small detachment which should be able to do the job over Cuba,
|
||
though at something less than the full design capability of the OXCART. The
|
||
goal was to operate at Mach 2.8 and 80,000 feet altitude.
|
||
|
||
(C) In order to meet the deadline set by General Carter, camera performance
|
||
would have to be validated, pilots qualified for Mach 2.8 flight, and
|
||
coordination with supporting elements arranged. Only one of several equip-
|
||
ments for electronic countermeasures (ECM) would be ready by November, and a
|
||
senior intra-governmental group, including representation from the President's
|
||
Scientific Advisory Committee, examined the problem of operating over Cuba
|
||
without the full complement of defensive systems. This panel decided that the
|
||
first few overflights could safely be conducted without them, but the ECM would
|
||
be necessary thereafter. The delivery schedule of ECM equipment was compatible
|
||
with this course of action.
|
||
|
||
(S) After considerable modifications to aircraft, the detachment simulated
|
||
Cuban missions on training flights, and a limited emergency SKYLARK capability
|
||
was announced on the date General Carter had set. With two weeks notice the
|
||
OXCART detachment could accomplish a Cuban overflight, though with fewer ready
|
||
aircraft and pilots than had been planned.
|
||
|
||
(S) During the following weeks the detachment concentrated on developing
|
||
SKYLARK into a sustained capability, with five ready pilots and five
|
||
operational aircraft. The main tasks were to determine aircraft range and
|
||
fuel consumption, attain repeatable reliable operation, finish pilot training,
|
||
prepare a family of SKYLARK missions, and coordinate routes with North American
|
||
Air Defense, Continental Air Defense, and the Federal Aviation Authority. All
|
||
this was accomplished without substantially hindering the main task of working
|
||
up OXCART to full design capability. We may anticipate the story, however, by
|
||
remarking that despite all this preparation the OXCART was never used over
|
||
Cuba. U-2's proved adequate, and the A-12 was reserved for more critical
|
||
situations.
|
||
|
||
(S) In 1965 a more critical situation did indeed emerge in Asia, and interest
|
||
in using the aircraft there began to be manifest. On 18 March 1965 Mr. McCone
|
||
discussed with Secretaries McNamara and Vance the increasing hazards to U-2
|
||
and drone reconnaissance of Communist China. A memorandum of this
|
||
conversation stated:
|
||
|
||
(S) "It was further agreed that we should proceed immediately with all
|
||
preparatory steps necessary to operate the OXCART over Communist
|
||
China, flying out of Okinawa. It was agreed that we should proceed
|
||
with all construction and related arrangements. However, this
|
||
decision did not authorize the deployment of the OXCART to Okinawa
|
||
nor the decision to fly the OXCART over Communist China. The decision
|
||
would authorize all preparatory steps and the expenditure of such
|
||
funds as might be involved. No decision has been taken to fly the
|
||
OXCART operationally over Communist China. This decision can only
|
||
be made by the President."
|
||
|
||
(S) Four days later Brigadier General Jack C. Ledford, Director of the Office
|
||
of Special Activities, DD/S&T, briefed Mr. Vance on the scheme which had
|
||
been drawn up for operations in the Far East. The project was called BLACK
|
||
SHIELD, and it called for the OXCART to operate out of the Kadena Air
|
||
Force Base in Okinawa. In the first phase, three aircraft would stage to
|
||
Okinawa for 60-day periods, twice a year, with about 225 personnel involved.
|
||
|
||
Msg#:17132 *AVIATION*
|
||
12/21/91 20:35:00 (Read 0 Times)
|
||
From: DEAN ADAMS
|
||
To: ALL
|
||
Subj: MORE OXCART
|
||
[ here is the 13th installment of this declassified OXCART history ]
|
||
|
||
(S)After this was in good order, BLACK SHIELD would advance to the point of
|
||
maintaining a permanent detachment at Kadena. Secretary Vance made $3.7
|
||
million available to be spent in providing support facilities on the island,
|
||
which were to be available by early fall of 1965.
|
||
|
||
(S) Meanwhile the Communists began to deploy surface-to-air missiles around
|
||
Hanoi, thereby threatening our current military reconnaissance capabilities.
|
||
Secretary McNamara called this to the attention of the Under Secretary of the
|
||
Air Force on 3 June 1965, and inquired about the practicability of substituting
|
||
OXCART aircraft for U-2's. He was told that BLACK SHIELD could operate over
|
||
Vietnam as soon as adequate aircraft performance was achieved.
|
||
|
||
(S) With deployment overseas thus apparently impending in the fall, the
|
||
detachment went into the final stages of its program for validating the
|
||
reliability of aircraft and aircraft systems. It set out to demonstrate
|
||
complete systems reliability at Mach 3.05 and at 2,300 nautical miles range,
|
||
with penetration altitude of 76,000 feet. A demonstrated capability for three
|
||
aerial refuelings was also part of the validation process.
|
||
|
||
(S) By this time the OXCART was well along in performance. The inlet, camera,
|
||
hydraulic, navigation, and flight control systems all demonstrated acceptable
|
||
reliability. Nevertheless, as longer flights were conducted at high speeds and
|
||
high temperatures, new problems came to the surface, the most serious being
|
||
with the electrical wiring system. Wiring connectors and components had to
|
||
withstand temperatures of more than 800 degrees Fahrenheit, together with
|
||
structural flexing, vibration, and shock. Continuing malfunctions in the inlet
|
||
controls, communications equipment, ECM systems, and cockpit instruments were
|
||
in many cases attributable to wiring failures. There was also disturbing
|
||
evidence that careless handling was contributing to electrical connector
|
||
failures. Difficulties persisted in the sealing of fuel tanks. What with one
|
||
thing and another, officials soon began to fear that the scheduled date for
|
||
BLACK SHIELD readiness would not be met. Prompt corrective action on the part
|
||
of Lockheed was in order. The quality of maintenance needed drastic improve-
|
||
ment. The responsibility for delivering an aircraft system with acceptable
|
||
reliability to meet an operational commitment lay in Lockheed's hands.
|
||
|
||
(S) In this uncomfortable situation, John Paragosky, Deputy for Technology,
|
||
OSA, went to the Lockheed plant to see Kelly Johnson on 3 August 1965. A frank
|
||
discussion ensued on the measures necessary to insure that BLACK SHIELD
|
||
commitments would be met, and Johnson concluded that he should himself spend
|
||
full time at the site in order to get the job done expeditiously. Lockheed
|
||
President Daniel Haughton offered the full support of the corporation, and
|
||
Johnson began duty at the site next day. His firm and effective management got
|
||
Project BLACK SHIELD back on schedule.
|
||
|
||
(S) Four primary BLACK SHIELD aircraft were selected and final validation
|
||
flights conducted. During these tests the OXCART achieved a maximum speed of
|
||
Mach 3.29, altitude of 90,000 feet, and sustained flight time above Mach 3.2 of
|
||
one hour and fourteen minutes. The maximum endurance flight lasted six hours
|
||
and twenty minutes. The last stage was reached on 20 November 1965, and two
|
||
days later Kelly Johnson wrote General Ledford:
|
||
|
||
(S) " ... Over-all, my considered opinion is that the aircraft can be
|
||
successfully deployed for the BLACK SHIELD mission with what I
|
||
would consider to be at least as low a degree of risk as in the
|
||
early U-2 deployment days. Actually, considering our performance
|
||
level of more than four times the U-2 speed and three miles more
|
||
operating altitude, it is probably much less risky than our first
|
||
U-2 deployment. I think the time has come when the bird should
|
||
leave its nest."
|
||
|
||
Msg#:17133 *AVIATION*
|
||
12/21/91 20:39:00 (Read 0 Times)
|
||
From: DEAN ADAMS
|
||
To: ALL
|
||
Subj: MORE OXCART
|
||
[ here is the 14th installment of this declassified OXCART history ]
|
||
|
||
(S) Ten days later the 303 Committee received a formal proposal that OXCART be
|
||
deployed to the Far East. The Committee, after examining the matter, did not
|
||
approve. It did agree, however, that short of actually moving aircraft to
|
||
Kadena all steps should be taken to develop and maintain a quick reaction
|
||
capability, ready to deploy within a 21-day period at any time after 1 January
|
||
1966.
|
||
|
||
(S) There the matter remained, for more than a year. During 1966 there were
|
||
frequent renewals of the request to the 303 Committee for authorization to
|
||
deploy OXCART to Okinawa and conduct reconnaissance missions over North
|
||
Vietnam, Communist China, or both. All were turned down. Among high officials
|
||
there was difference of opinion; CIA, the Joint Chiefs of Staff, and the
|
||
Presidents Foreign Intelligence Advisory Board favored the move, while Alexis
|
||
Johnson representing State, and Defense in the persons of Messrs. McNamara and
|
||
Vance, opposed it. The proponents urged the necessity of better intelligence,
|
||
especially on a possible Chinese Communist build-up preparatory to intervention
|
||
in Vietnam. The opponents felt that better intelligence was not so urgently
|
||
needed as to justify the political risks of basing the aircraft in Okinawa and
|
||
thus almost certainly disclosing to Japanese and other propagandists. They
|
||
also believed it undesirable to use OXCART and reveal something of its
|
||
capability until a more pressing requirement appeared. At least once, on 12
|
||
August 1966, the divergent views were brought up to the President, who
|
||
confirmed the 303 Committee's majority opinion against deployment.
|
||
|
||
(S) Meanwhile, of course, flight testing and crew proficiency training
|
||
continued. There was plenty of time to improve mission plans and flight
|
||
tactics, as well as to prepare the forward area at Kadena. New plans shortened
|
||
deployment time from the 21 days first specified. Personnel and cargo were to
|
||
be airlifted to Kadena the day deployment was approved. On the fifth day the
|
||
first OXCART would depart and travel the 6,673 miles in five hours and 34
|
||
minutes. The second would go on the seventh and the third on the ninth day.
|
||
The first two would be ready for an emergency mission on the eleventh day, and
|
||
for a normal mission on the fifteenth day.
|
||
|
||
(S) An impressive demonstration of the OXCART's capability occurred on 21
|
||
December 1966 when Lockheed test pilot Bill Park flew 10,198 statute miles in
|
||
six hours. The aircraft left the test area in Nevada and flew northward over
|
||
Yellowstone National Park, thence eastward to Bismark, North Dakota, and on to
|
||
Duluth, Minnesota. It then turned south and passed Atlanta en route to Tampa,
|
||
Florida, then northwest to Portland, Oregon, then southwest to Nevada. Again
|
||
the flight turned eastward, passing Denver and St. Louis. Turning around at
|
||
Knoxville, Tennessee, it passed Memphis in the home stretch back to Nevada.
|
||
This flight established a record unapproachable by any other aircraft; it began
|
||
at about the same time a typical government employee starts his work day and
|
||
ended two hours before his quitting time.
|
||
|
||
(S) Shortly after this exploit, tragedy befell the program. During a routine
|
||
training flight on 5 January 1967, the fourth aircraft was lost, together with
|
||
its pilot. The accident occurred during descent about 70 miles from the base.
|
||
A fuel guage failed to function properly, and the aircraft ran out of fuel
|
||
only minutes before landing. The pilot, Walter Ray, ejected but was killed
|
||
when he failed to separate from the ejection seat before impact. The aircraft
|
||
was totally destroyed. Its wreckage was found on 6 January and Ray's body
|
||
recovered a day later. Through Air Force channels a story was released to the
|
||
effect that an Air Force SR-71, on a routine test flight out of Edwards Air
|
||
Force Base, was missing and presumed down in Nevada. The pilot was identified
|
||
as a civilian test pilot, and the newspapers connected him with Lockheed.
|
||
Flight activity at the base was again suspended during investigation of the
|
||
causes both for the crash and for the failure of the seat separation device.
|
||
|
||
(S) It is worth observing that none of the four accidents occurred in the
|
||
high-Mach-number, high-temperature regime of flight. All involved traditional
|
||
problems inherent in any aircraft. In fact, the OXCART was by this time
|
||
performing at high speeds, with excellent reliability.
|
||
|
||
Msg#:18396 *AVIATION*
|
||
12/23/91 01:47:00 (Read 0 Times)
|
||
From: DEAN ADAMS
|
||
To: ALL
|
||
Subj: REPLY TO MSG# 18392 (MORE OXCART)
|
||
[ here is the 15th installment of this declassified OXCART history ]
|
||
|
||
(S) * Neither on this nor on other flights was there much trouble from sonic
|
||
boom. To be sure, the inhabitants of a small village some 30 miles from the
|
||
site were troubled as the aircraft broke through the sound barrier while
|
||
gaining altitude. A change of course remedied this. At altitude OXCART
|
||
produced no more than an ominous rumble on the ground and since the plane
|
||
was invisible to the naked eye no one associated this sound with its actual
|
||
source.
|
||
|
||
(S) BLACK SHIELD
|
||
|
||
(S) About May of 1967 prospects for deployment took a new turn. A good deal
|
||
of apprehension was evident in Washington about the possibility that the
|
||
Communists might introduce surface-to-surface missiles into North Vietnam,
|
||
and concern was aggravated by doubts as to whether we could detect such a
|
||
development if it occurred. The President asked for a proposal on the matter;
|
||
CIA briefed the 303 Committee and once again suggested that the OXCART be used.
|
||
Its camera was far superior to those on drones or on the U-2, its vulnerability
|
||
was far less. The State and Defense members of the Committee decided to
|
||
re-examine the requirements and the political risks involved. While they were
|
||
engaged in their deliberations, Director of Central Intelligence, Richard
|
||
Helms, submitted to the 303 Committee another formal proposal to deploy the
|
||
OXCART. In addition, he raised the matter at President Johnson's "Tuesday
|
||
lunch" on 16 May, and received the Presidents approval to "go." Walt Rostow
|
||
later in the day formally conveyed the President's decision, and the BLACK
|
||
SHIELD deployment plan was forthwith put into effect.
|
||
|
||
(S) On 17 May airlift to Kadena began. On 22 May the first A-12 (Serial No.
|
||
131) flew nonstop to Kadena in six hours and six minutes. Aircraft No. 127
|
||
departed on 24 May and arrived at Kadena five hours and 55 minutes later.
|
||
The third, No. 129, left according to plan on 26 May 1967 and proceeded
|
||
normally until in the vicinity of Wake Island where the pilot experienced
|
||
difficulties with the inertial navigation and communications systems. In the
|
||
circumstances, he decided to make a precautionary landing at Wake Island. The
|
||
prepositioned emergency recovery team secured the aircraft without incident and
|
||
the flight to Kadena resumed next day.
|
||
|
||
(C) Arrangements were made to brief the Ambassadors and Chiefs of Station in
|
||
the Philippines, Formosa, Thailand, South Vietnam, and Japan, and the High
|
||
Commissioner and Chief of Station, Okinawa. The Prime Ministers of Japan and
|
||
Thailand were advised, as were the President and Defense Minister of the
|
||
Republic of China. The Chiefs of the Air Force of Thailand and the Republic
|
||
of China were also briefed. Reactions were favorable.
|
||
|
||
(S) On 29 May 1967, the unit at Kadena was ready to fly an operational mission.
|
||
Under the command of Colonel Hugh C. Slater two hundred and sixty personnel had
|
||
deployed to the BLACK SHIELD facility. Except for hangars, which were a month
|
||
short of completion, everything was in shape for sustained operations. Next
|
||
day the detachment was alerted for a mission on 31 May, and the moment arrived
|
||
which would see the culmination of ten years of effort, worry, and cost. As
|
||
fate would have it, on the morning of the 31st heavy rain fell at Kadena. Since
|
||
weather over the target area was clear, preparations continued in hopes that
|
||
the local weather would clear. When the time for take-off approached, the
|
||
OXCART, which had never operated in heavy rain, taxied to the runway, and took
|
||
off while the rain continued.
|
||
|
||
(S) The first BLACK SHIELD mission followed one flight line over North Vietnam
|
||
and one over the Demilitarized Zone. It lasted three hours and 39 minutes,
|
||
and the cruise legs were flown at Mach 3.1 and 80,000 feet. Results were
|
||
satisfactory. Seventy of the 190 known SAM sites in North Vietnam were photo-
|
||
graphed, as were nine other priority targets. There were no radar signals
|
||
detected, indicating that the first mission had gone completely unnoticed by
|
||
both Chinese and North Vietnamese.
|
||
|
||
Msg#:18397 *AVIATION*
|
||
12/23/91 01:53:00 (Read 0 Times)
|
||
From: DEAN ADAMS
|
||
To: ALL
|
||
Subj: REPLY TO MSG# 18396 (MORE OXCART)
|
||
[ here is the 16th installment of this declassified OXCART history ]
|
||
|
||
(S) Fifteen BLACK SHIELD missions were alerted during the period from 31 May to
|
||
15 August 1967. Seven of the fifteen were flown and of these, four detected
|
||
radar tracking signals, but no hostile action was taken against any of them. By
|
||
mid-July they had determined with a high degree of confidence that there were
|
||
no surface-to-surface missiles in North Vietnam.
|
||
|
||
(C) All operational missions were planned, directed, and controlled by Project
|
||
Headquarters in Washington. A constant watch was maintained on the weather in
|
||
the target areas. Each day at a specified hour (1600 hours local) a mission
|
||
alert briefing occurred. If the forecast weather appeared favorable, the
|
||
Kadena base was alerted and provided a route to be flown. The alert preceded
|
||
actual take-off by 28 to 30 hours. Twelve hours prior to take-off (H minus 12)
|
||
a second review of target weather was made. If it continued favorable, the
|
||
mission generation sequence continued. At H minus 2 hours, a "go-no-go"
|
||
decision was made and communicated to the field. The final decision, it should
|
||
be noted, depended not solely on weather in the target area; conditions had to
|
||
be propitious also in the refueling areas and at the launch and recovery base.
|
||
|
||
(C) Operations and maintenance at Kadena began with the receipt of alert
|
||
notification. Both a primary aircraft and pilot and a back-up aircraft and
|
||
pilot were selected. The aircraft were given thorough inspection and servicing,
|
||
all systems were checked, and the cameras loaded into the aircraft. Pilots
|
||
received a detailed route briefing in the early evening prior to the day of
|
||
flight. On the morning of the flight a final briefing occurred, at which time
|
||
the condition of the aircraft and its systems was reported, last-minute weather
|
||
forecasts reviewed, and other relevant intelligence communicated together with
|
||
any amendments or changes in the flight plan. Two hours prior to take-off the
|
||
primary pilot had a medical examination, got into his suit, and was taken to
|
||
the aircraft. If any malfunctions developed on the primary aircraft, the
|
||
back-up could execute the mission one hour later.
|
||
|
||
(S) A typical route profile for a BLACK SHIELD mission over North Vietnam
|
||
included a refueling shortly after take-off, south of Okinawa, the planned
|
||
photographic pass or passes, withdrawl to a second aerial refueling in the
|
||
Thailand area, and return to Kadena. So great was the OXCART's speed that
|
||
it spent only 12 1/2 minutes over North Vietnam in a typical "single pass"
|
||
mission, or a total of 21 1/2 minutes on two passes. Its turning radius of
|
||
86 miles was such, however, that on some mission profiles it might be forced
|
||
during its turn to intrude into Chinese airspace.
|
||
|
||
(S) Once landed back at Kadena, the camera film was removed from the aircraft,
|
||
boxed, and sent by special plane to the processing facilities. Film from
|
||
earlier missions was developed at the Eastman Kodak plant in Rochester, New
|
||
York. By late summer an Air Force Center in Japan carried out the processing
|
||
in order to place the photointelligence in the hands of American commanders
|
||
in Vietnam within 24 hours of completion of a BLACK SHIELD mission.
|
||
|
||
(S) Between 16 August and 31 December 1967, twenty-six missions were alerted.
|
||
Fifteen were flown. On 17 December one SAM site tracked the vehicle with its
|
||
acquisition radar but was unsuccessful with its Fan Song guidance radar. On
|
||
28 October a North Vietnamese SAM site for the first time launched a single,
|
||
albiet unsuccessful, missile at the OXCART. Photography from this mission
|
||
documented the event with photographs of missile smoke above the SAM firing
|
||
site, and with pictures of the missile and of its contrail. Electronic
|
||
countermeasures equipment appeared to perform well against the missile firing.
|
||
|
||
(S) During the flight of 30 October 1967, pilot Dennis Sullivan detected radar
|
||
tracking on his first pass over North Vietnam. Two sites prepared to launch
|
||
missiles but neither did. During the second pass at least six missiles were
|
||
fired at the OXCART, each confirmed by missile vapor trails on mission photo-
|
||
graphy. Sullivan saw these vapor trails and witnessed three missile detonations.
|
||
Post-flight inspection of the aircraft revealed that a piece of metal had
|
||
penetrated the lower right wing fillet area and lodged against the support
|
||
structure of the wing tank. The fragment was not a warhead pellet but may have
|
||
been a part of the debris from one of the missile detonations observed by the
|
||
pilot.
|
||
|
||
Msg#:18398 *AVIATION*
|
||
12/23/91 01:58:00 (Read 0 Times)
|
||
From: DEAN ADAMS
|
||
To: ALL
|
||
Subj: REPLY TO MSG# 18397 (MORE OXCART)
|
||
[ here is the 17th installment of this declassified OXCART history ]
|
||
|
||
(C) Between 1 January and 31 March 1968 six missions were flown out of fifteen
|
||
alerted. Four of these were over North Vietnam and two over North Korea. The
|
||
first mission over North Korea on 26 January occurred during a very tense period
|
||
following seizure of the Pueblo on the 23rd. The aim was to discover whether
|
||
the North Koreans were preparing any large scale hostile move on the heels of
|
||
this incident. Chinese tracking of the flight was apparent, but no missiles
|
||
were fired at the plane.
|
||
|
||
(C) The Department of State was reluctant to endorse a second mission over
|
||
North Korea for fear of the diplomatic repercussions which could be expected
|
||
if the aircraft came down in hostile territory. Brigadier General Paul Bacalis
|
||
then briefed Secretary Rusk on the details and objectives of the mission, and
|
||
assured him that the aircraft would transit North Korea in no more than seven
|
||
minutes. He explained that even if some failure occurred during flight the
|
||
aircraft would be highly unlikely to land either in North Korea or in China.
|
||
Secretary Rusk made suggestions to alter the flight plan, thus becoming the
|
||
projects highest ranking flight planner. Between 1 April and 9 June 1968 two
|
||
missions were alerted for North Korea. Only the mission which flew on 8 May
|
||
was granted approval.
|
||
|
||
(S) The SR-71
|
||
|
||
(S) All through the OXCART program the Air Force had been exceedingly helpful.
|
||
It gave financial support, conducted the refueling program, provided
|
||
operational facilities at Kadena, and air-lifted OXCART personnel and supplies
|
||
to Okinawa for the operations over Vietnam and North Korea. It also ordered
|
||
from Lockheed a small fleet of A-11's, which upon being finished as two seated
|
||
reconnaissance aircraft would be named SR-71. These would become operational
|
||
about 1967.
|
||
|
||
(S) The stated mission of the SR-71 was to conduct "post-strike reconnais-
|
||
sance," that is, to look the enemy situation over after a nuclear exchange.
|
||
The likelihood of using the aircraft in the capacity hardly appeared great, but
|
||
SR-71 was of course also capable of ordinary intelligence missions. For these
|
||
purposes, however, the OXCART possessed certain clear advantages. It carried
|
||
only one man, and largely for this reason it had room for a much bigger and
|
||
better camera, as well as for various other collection devices which at the
|
||
time could not be carried by the SR-71. It was certainly the most effective
|
||
reconnaissance aircraft in existence, or likely to be in existence for years to
|
||
come. Also it was operated by civilians, and could be employed covertly, or at
|
||
least without the number of personnel and amount of fanfare normally attending
|
||
an Air Force operation.
|
||
|
||
(S) The fact the SR-71's were ordered eased the path of OXCART development,
|
||
since it meant that the financial burden was shared with the Air Force, and the
|
||
cost per aircraft was somewhat reduced by producing greater numbers. In the
|
||
longer run, however, the existence of SR-71 spelled the doom of OXCART, for
|
||
reasons which appear to have been chiefly financial and in a manner now to be
|
||
related.
|
||
|
||
(S) Ending
|
||
|
||
(S) During November 1965, the very month when OXCART was finally declared
|
||
operational, the moves toward its demise commenced. Within the Bureau of the
|
||
Budget a memorandum was circulated expressing concern at the costs of the A-12
|
||
and SR-71 programs, both past and projected. It questioned the requirement for
|
||
the total number of aircraft represented in the combined fleets, and doubted
|
||
the necessity for a separate CIA (OXCART) fleet. Several alternatives were
|
||
proposed to achieve a substantial reduction in the forecasted spending, but the
|
||
recommended course was to phase out the A-12 program by September 1966 and stop
|
||
any further procurement of SR-71 aircraft. Copies of this memorandum were
|
||
sent to the Department of Defense and the CIA with the suggestion that those
|
||
agencies explore the alternatives set out in the paper. But the Secretary of
|
||
Defense declined to consider the proposal, presumably because the SR-71 would
|
||
not be operational by September 1966.
|
||
|
||
Msg#:18399 *AVIATION*
|
||
12/23/91 02:02:00 (Read 0 Times)
|
||
From: DEAN ADAMS
|
||
To: ALL
|
||
Subj: REPLY TO MSG# 18398 (MORE OXCART)
|
||
[ here is the 18th installment of this declassified OXCART history ]
|
||
|
||
(S) Things remained in this state until in July 1966 the Bureau of the Budget
|
||
proposed that a study group be established to look into the possibility of
|
||
reducing expenses on the OXCART and SR-71 programs. The group was requested to
|
||
consider the following alternatives:
|
||
|
||
1. Retention of separate A-12 and SR-71 fleets, i.e., status quo.
|
||
2. Collocation of the two fleets.
|
||
3. Transfer of the OXCART mission and aircraft to SAC.
|
||
4. Transfer of the OXCART mission to SAC and storage of A-12 aircraft.
|
||
5. Transfer of the OXCART mission to SAC and disposal of A-12 aircraft.
|
||
|
||
(S)The study group included C. W. Fischer, Bureau of the Budget; Herbert
|
||
Bennington, Department of Defense; and John Paragosky, Central Intelligence
|
||
Agency.
|
||
|
||
(S) This group conducted its study through the fall of 1966, and identified
|
||
three principal alternatives of its own. They were:
|
||
|
||
1. To maintain the status quo and continue both fleets at current
|
||
approval levels.
|
||
|
||
2. To mothball all A-12 aircraft, but maintain the OXCART capability
|
||
by sharing SR-71 aircraft between SAC and CIA.
|
||
|
||
3. To terminate the OXCART fleet in January 1968 (assuming an
|
||
operational readiness date of September 1967 for the SR-71) and
|
||
assign all missions to the SR-71 fleet.
|
||
|
||
(S) On 12 December 1966 there was a meeting at the Bureau of the Budget
|
||
attended by Mr. Helms, Mr. Shultze, Mr. Vance, and Dr. Hornig, Scientific
|
||
Advisor to the President. Those present voted on the alternatives proposed in
|
||
the Fischer-Bennington-Paragosky report. Messrs. Vance, Schultze, and Hornig
|
||
chose to terminate the OXCART fleet, and Mr. Helms stood out for eventual
|
||
sharing of the SR-71 fleet between CIA and SAC. The Bureau of the Budget
|
||
immediately prepared a letter to the President setting forth the course of
|
||
action recommended by the majority. Mr. Helms, having dissented from the
|
||
majority, requested his Deputy Director for Science and Technology to prepare
|
||
a letter to the President stating CIA's reasons for remaining in the
|
||
reconnaissance business.
|
||
|
||
(S) On 16 December Mr. Schultze handed Mr. Helms a draft memorandum to the
|
||
President which requested a decision either to share the SR-71 fleet between
|
||
CIA and SAC, or to terminate the CIA capability entirely. This time Mr. Helms
|
||
replied that new information of considerable significance had been brought to
|
||
his attention concerning SR-71 performance. He requested another meeting after
|
||
1 January to review pertinent facts, and also asked that the memorandum to the
|
||
President be withheld pending that meeting's outcome. Specifically, he cited
|
||
indications that the SR-71 program was having serious technical problems and
|
||
that there was real doubt that it would achieve an operational capability by
|
||
the time suggested for termination of the A-12 program. Mr. Helms therefore
|
||
changed his position from sharing the SR-71 aircraft with SAC to a firm
|
||
recommendation to retain the OXCART A-12 fleet under civilian sponsorship. The
|
||
Budget Bureau's memorandum was nevertheless transmitted to the President, who
|
||
on 28 December 1966 accepted the recommendations of Messrs. Vance, Hornig, and
|
||
Schultze, and directed the termination of the OXCART Program by 1 January 1968.
|
||
|
||
(S) This decision meant that a schedule had to be developed for orderly
|
||
phase-out. After consultation with project Headquarters, the Deputy Secretary
|
||
of Defense was advised on 10 January 1967 that four A-12's would be placed
|
||
in storage in July 1967, two more by December, and the last four by the end
|
||
of January 1968. In May Mr. Vance directed that the SR-71 assume contingency
|
||
responsibility to conduct Cuban overflights as of 1 July 1967 and take over
|
||
the dual capability over Southeast Asia and Cuba by 1 December 1967. This
|
||
provided for some overlap between OXCART withdrawal and SR-71 assumption of
|
||
responsibility.
|
||
|
||
Msg#:18400 *AVIATION*
|
||
12/23/91 02:04:00 (Read 0 Times)
|
||
From: DEAN ADAMS
|
||
To: ALL
|
||
Subj: REPLY TO MSG# 18399 (MORE OXCART)
|
||
[ here is the 19th installment of this declassified OXCART history ]
|
||
|
||
(S) Meanwhile until 1 July 1967 the OXCART Detachment was to maintain its
|
||
capability to conduct operational missions both from a prepared location
|
||
overseas and from the US. This included a 15 day quick reaction capability for
|
||
deployment to the Far East and a seven-day quick reaction for deployment over
|
||
Cuba. Between 1 July and 31 December 1967 the fleet would remain able to
|
||
conduct operational missions either from a prepared overseas base or from home
|
||
base, but not from both simultaneously. A quick reaction capability for either
|
||
Cuban overflights or deployment to the Far East would also be maintained.
|
||
|
||
(S) All these transactions and arrangements occurred before the OXCART had
|
||
conducted a single operational mission or even deployed to Kadena for such a
|
||
mission. As recounted above, the aircraft first performed its appointed role
|
||
over North Vietnam on the last day of May 1967. In succeeding months it
|
||
demonstrated both its exceptional technical capabilities and the competence
|
||
with which its operations were managed. As word began to get around that
|
||
OXCART was to be phased out, high officials commenced to feel some disquiet.
|
||
Concern was shown by Walt Rostow, the President's Special Assistant; by key
|
||
Congressional figures, members of the President's Foreign Intelligence Advisory
|
||
Board, and the President's Scientific Advisory Committee. The phase-out
|
||
lagged, and the question was reopened.
|
||
|
||
(S) A new study of the feasibility and cost of continuing the OXCART program
|
||
was completed in the spring of 1968 and four new alternatives were proposed:
|
||
|
||
1. Transfer all OXCART aircraft to SAC by 31 October 1968; substitute
|
||
Air Force for contractor support where possible; turn the test A-12
|
||
aircraft over to the SR-71 test facility.
|
||
|
||
2. Transfer OXCART as in alternative 1, above, and store eight SR-71's.
|
||
|
||
3. Close the OXCART home base and collocate the fleet with SR-71's at
|
||
Beale Air Force Base in California, but with CIA retaining control
|
||
and management.
|
||
|
||
4. Continue OXCART operations at its own base under CIA control and
|
||
management.
|
||
|
||
(S) Mr. Helms expressed his reactions to these alternatives in a memorandum to
|
||
Messrs. Nitze, Hornig, and Flax, dated 18 April 1968. In it he questioned why,
|
||
if eight SR-71's could be stored in one option, they could not be stored in all
|
||
the options, with the resultant savings applied in each case. He questioned
|
||
the lower cost figures of combining the OXCART with the SR-71's and disagreed,
|
||
for security reasons, with collocating the two fleets. Above all, however, he
|
||
felt that the key point was the desirability of retaining a covert reconnais-
|
||
sance capability under civilian management. It was his judgement that such a
|
||
requirement existed, and he recommended that OXCART continue at its own base
|
||
under CIA management.
|
||
|
||
(S) In spite of all these belated efforts, the Secretary of Defense on 16 May
|
||
1968 reaffirmed the original decision to terminate the OXCART Program and
|
||
store the aircraft. At his weekly luncheon with his principal advisors on 21
|
||
May 1968, the President confirmed Secretary Clifford's decision.
|
||
|
||
(S) Early in March 1968, USAF SR-71 aircraft began to arrive at Kadena to take
|
||
over the BLACK SHIELD commitment, and by gradual stages the A-12 was placed on
|
||
standby to back up the SR-71. The last operational mission flown by OXCART was
|
||
on 8 May 1968 over North Korea, following which the Kadena Detachment was
|
||
advised to prepare to go home. Project Headquarters selected 8 June 1968 as
|
||
the earliest possible date to begin redeployment, and in the meantime flights
|
||
of A-12 aircraft were to be limited to those essential for maintaining flying
|
||
safety and pilot proficiency. After BLACK SHIELD aircraft arrived in the US
|
||
they would proceed to storage. Those already at base were placed in storage by
|
||
7 June.
|
||
|
||
Msg#:18401 *AVIATION*
|
||
12/23/91 02:07:00 (Read 0 Times)
|
||
From: DEAN ADAMS
|
||
To: ALL
|
||
Subj: REPLY TO MSG# 18400 (MORE OXCART)
|
||
[ here is the 20th/LAST installment of this declassified OXCART history ]
|
||
|
||
(S) During its final days overseas the OXCART enterprise suffered yet another
|
||
blow, as inexplicable as it was tragic. On 4 June Aircraft No. 129, piloted
|
||
by Jack Weeks, set out from Kadena on a check flight necessitated by a change
|
||
of engine. Weeks was heard from when 520 miles east of Manila. Then he
|
||
disappeared. Search and rescue operations found nothing. No cause for the
|
||
accident was ever ascertained, and it remains a mystery to this day. Once
|
||
again the official news release identified the lost aircraft as an SR-71 and
|
||
security was maintained. A few days afterwards the two remaining planes on
|
||
Okinawa flew to the US and were stored with the remainder of the OXCART family.
|
||
|
||
(S) Postscript
|
||
|
||
(S) In summary; the OXCART Program lasted just over ten years, from its
|
||
inception in 1957 through first flights in 1962 to termination in 1968.
|
||
Lockheed produced 15 OXCARTS, three YF-12A's and 31 SR-71's. The 49 supersonic
|
||
aircraft had completed more than 7,300 flights, with 17,000 hours in the air.
|
||
Over 2,400 hours had been above Mach 3. Five OXCART's were lost in accidents;
|
||
two pilots were killed, and two had narrow escapes. In addition, two F-101
|
||
chase planes were lost with their Air Force pilots during OXCART's testing
|
||
phase.
|
||
|
||
(U) The main objective of the program-to create a reconnaissance aircraft of
|
||
unprecedented speed, range, and altitude capability-was triumphantly achieved.
|
||
It may well be, however, that the most important aspects of the effort lay
|
||
in its by-products--the notable advances in aerodynamic design, engine
|
||
performance, cameras, electronic countermeasures, pilot life support systems,
|
||
antiair devices, and above all in milling, machining, and shaping titanium.
|
||
Altogether it was a pioneering accomplishment.
|
||
|
||
(S) In a ceremony at the Nevada base on 26 June 1968, Vice Admiral Rufus L.
|
||
Taylor, Deputy Director of Central Intelligence, presented the CIA Intelligence
|
||
Star for valor to pilots Kenneth S. Collins, Ronald L. Layton, Francis J.
|
||
Murray, Dennis B. Sullivan, and Mele Vojvodich for participation in the BLACK
|
||
SHIELD operation. The posthumous award to pilot Jack W. Weeks was accepted by
|
||
his widow. The United States Air Force Legion of Merit was presented to Colonel
|
||
Slater and his Deputy, Colonel Maynard N. Amundson. The Air Force Outstanding
|
||
Unit Award was presented to the members of the OXCART Detachment (1129th
|
||
Special Activities Squadron, Detachment 1) and the USAF supporting units.
|
||
|
||
(U) Wives of the pilots were present and learned for the first time of the
|
||
activities in which their husbands had been involved. Kelly Johnson was a
|
||
guest speaker at the ceremony, and lamented in moving words the end of an
|
||
enterprise which had marked his most outstanding achievement in aircraft
|
||
design. His own awards had already been received: The Presidents Medal of
|
||
Freedom in 1964, and on 10 February 1966, the National Medal of Science,
|
||
from President Johnson, for his contributions to aerospace science and to
|
||
the national security.
|
||
UNCLASSIFIED
|
||
|
||
Msg#:18402 *AVIATION*
|
||
12/23/91 02:13:00 (Read 0 Times)
|
||
From: DEAN ADAMS
|
||
To: ALL
|
||
Subj: NO MORE OXCART!
|
||
OK... Now you have it ALL! This document took -20- Fido messages to post in
|
||
it's entirety, but I think it was worth it... Enjoy!
|
||
* Origin: SLC-6 Western Spaceport in Simi Valley, CA (1:102/1006.4)
|
||
|
||
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|
||
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|
||
Msg#:17181 *AVIATION*
|
||
12/22/91 23:15:57 (Read 0 Times)
|
||
From: ALBERT DOBYNS
|
||
To: ALL
|
||
Subj: AF SERIAL NUMBERING
|
||
Several years ago I read in a book on USAF planes 1945-1956 that the Air Force
|
||
has a numbering scheme that goes something like this: the number that appears
|
||
on the tail usually starts with the last digit of the year it was made followed
|
||
by the rest of the number. The full number is usually painted on in small
|
||
numbers near the cockpit and it contains the year in 2 digit form plus the
|
||
remainder of the number. For example a YF-12 with a tail number of 06935 would
|
||
have a full number of 60-6935 where 60 is the year is was built (after adding
|
||
1900 to it of course!). Looking at SR-71 numbers on the tail one would/could
|
||
expect the same thing to apply. SR-71B has a tail number of 17956 which led me
|
||
to believe that its full number would have been 61-7956. But all the books I
|
||
have list the full numbers as 64-179xx. OK so I got used to thinking of it
|
||
that way. Then I happened to notice in a few pictures that have those red
|
||
protective covers on the cockpit windows that the number painted on it is
|
||
61-7956 for example. Now I'm confused. Can any of our resident military
|
||
flyers make sense out of this? Perhaps the AF decided to change the SR-71s
|
||
number to have it start with 64 but didn't want to spend money changing items
|
||
that had the old numbering scheme on them. ps: many thanks to Dean Adams for
|
||
posting that Oxcart info! After all his info is on the network, I promise I'll
|
||
try to get Dean (and myself) to write a note that doesn't talk about the
|
||
Blackbirds! <grins>
|
||
|
||
Msg#:17332 *AVIATION*
|
||
12/21/91 13:43:25 (Read 0 Times)
|
||
From: BILL HODGES
|
||
To: IVAN BAIRD
|
||
Subj: OX S(OMETHING?)?
|
||
IB> I am at least on person who is extremely intrested in Aviation (especially
|
||
IB> 'Black Stuff') and who gets his information, not only from this echo, a
|
||
IB> mailing list on the Internet called Skunk-Works.
|
||
IB> ^^^^^^^^ ^^^^^^^^^^^
|
||
|
||
I'm not familiar with "that". Is it Aviation related? Flying Saucer? Science
|
||
Fiction? Trekkies?
|
||
|
||
IB > ..a recently declassified document on the Oxcart Project.
|
||
|
||
Why do you think there ever was a classified CIA document of the nature you
|
||
indicate? How do you know there was an "Oxcart"? How do you know the document
|
||
was declassified? Anyone seen it? Isn't it strange that no reputable or
|
||
scandalous radio, TV, Cable, program nor newspaper, flyer, scandal sheet,
|
||
magazine, or book published this inside story? Did anyone try to find the
|
||
originator of first BBS disclosure of this _______ ? Does anyone ever consider
|
||
authentication from a reliable person? In case you hadn't guessed, I think
|
||
this is a hoax.
|
||
|
||
Msg#:17333 *AVIATION*
|
||
12/21/91 13:44:49 (Read 0 Times)
|
||
From: BILL HODGES
|
||
To: DEAN ADAMS
|
||
Subj: REPLY TO MSG# 17332 (OX S(OMETHING?)?)
|
||
DA > Here is the first part of a 25 page document written
|
||
DA > by the CIA, about the development of the A-12 Blackbird and
|
||
^^^^^^^^^^
|
||
Why do you think so?
|
||
Who authenticated? Does typing on an echo make it true?
|
||
|
||
DA > Document downgraded to < Unclassified > 25 Feb 91
|
||
DA > IAW Senior Crown Security Class Guide, dated 11/01/89
|
||
DA > -------------------------------------------------------
|
||
DA > (S) THE OXCART STORY
|
||
DA > Thomas P. McIninch
|
||
|
||
Has anyone even questioned the format or manner of expression? Is "Senior.....
|
||
Guide" the senior class at Oxford University? Who is Thomas P. McIninch?
|
||
Everybody in Govt has a title. It is my opinion this document was written by
|
||
some college kids who are unfamiliar with US Government grammar, use of
|
||
acronyms, stilted manner, etc. There are several gross errors in the parts
|
||
so far posted. If this were a real CIA document, we would all probably be
|
||
speaking Russian long ago due to their ineptness. By the time you have posted
|
||
the whole thing, I think it will be evident to all (at least those over 30) it
|
||
is a hoax. If there are still some believers left, I will compose a 100%
|
||
genuine placebo message regarding this OxS.. message. Author will be Lt.Gen.
|
||
P.T.Barnum who was CIA Director of USAF affairs. Date will be 1 Apr 1991 and I
|
||
will declassify it from Top Secret crypto Eyes Only to Before Secret (BS). It
|
||
will say whatever it takes to convince the believers that they were taken in.
|
||
Like Frank said. You didn't write it. You are just distributing it as asked
|
||
here.
|
||
|
||
Msg#:17334 *AVIATION*
|
||
12/21/91 13:47:50 (Read 0 Times)
|
||
From: BILL HODGES
|
||
To: MIKE LECLAIR
|
||
Subj: REPLY TO MSG# 16432 (SR-71 BLACKBIRD)
|
||
In a 20 Dec message to Bob Cadwalader:
|
||
ML> I don't follow you when you say my assumptions on the YF-12A are unfounded
|
||
ML> .....It WASN'T designed or developed to be an interceptor or fighter...
|
||
|
||
Are you mistaking YF-12A for SR-71? Ever hear of the A-11? Ever hear of the
|
||
"Improved Manned Interceptor" program? "...A-11 originally designed as follow
|
||
on to U-2..the three A-11s, (sn 60-6934 to 6936)....Later they were completed
|
||
as YF-12A research aircraft in the Improved Manned Interceptor program,
|
||
carrying Hughes ASG-18 pulse doppler radar, infra-red sensors and eight Hughes
|
||
AIM-47A large long-range air-to-air missiles in an internal bay."
|
||
[Encyclopedia of the World's Combat Aircraft, Bill Gunston]
|
||
|
||
"The original A-11 shape.....The first three aircraft (60-6934/6) were built as
|
||
YF-12A research interceptors, with a pressurized cockpit for a pilot and air
|
||
interception officer. Hughes ASG-18 pulse-doppler radar,...tandem missile bays
|
||
for (usually) eight AIM-47 AAMs...." [Modern US War Machine]
|
||
|
||
These were both written before latest release of a lot of previously classified
|
||
information but I do remember the A-11 and IMI program. You can't lump the
|
||
SR-71 (RS-71) in with YF-12, A-11/A-12 any more than you can lump the B-707,
|
||
C-135, KC-135, VC-137, and E-3A together as "designed as a......." and have it
|
||
cover all.
|
||
|
||
Msg#:18734 *AVIATION*
|
||
12/23/91 22:48:00 (Read 0 Times)
|
||
From: DEAN ADAMS
|
||
To: BILL HODGES
|
||
Subj: RE: OX
|
||
DA>> Here is the first part of a 25 page document written
|
||
DA>> by the CIA, about the development of the A-12 Blackbird and
|
||
|
||
BH> Why do you think so?
|
||
|
||
The "CIA" part I am not that concerned about, BUT the events described in GREAT
|
||
and very accurate detail are all about the project which WAS under CIA control.
|
||
Who else should write a history about it?
|
||
|
||
BH> Who authenticated?
|
||
|
||
Quite a few people with the ability to know.
|
||
|
||
BH> Does typing on an echo make it true?
|
||
|
||
No, that lets more people benefit from reading it. This copy originated from
|
||
people connected with setting up the A-12/D-21 exhibit at the Seattle Museum of
|
||
Flight. I believe the man who gave it out was Ben Rich, but also in attendance
|
||
were: Keith Beswick (Bill Park's LCO on many D-21A drone launches), Brigadier
|
||
General Buck Adams (a former SR-71 pilot), Jerry Miller (First Marquardt
|
||
representative for the D-21A and D-21B programs at Groom and Beale), James
|
||
Walborn (Honeywell Flight Systems, was involved in the flight systems for the
|
||
A-12's at Groom), etc...
|
||
|
||
BH> Has anyone even questioned the format or manner of expression?
|
||
|
||
Such as? It is clearly a general historical summary, certainly not any kind of
|
||
technical document.
|
||
|
||
BH> Is "Senior.....Guide" the senior class at Oxford University?
|
||
|
||
Funny. "Senior Crown" *IS* a valid classification level. This was confirmed
|
||
by a person who HAS the same clearance and currently works at NASA Ames-Dryden.
|
||
|
||
BH> Who is Thomas P. McIninch? Everybody in Govt has a title.
|
||
|
||
He is -supposed- to be an author for the CIA, but I don't have any more
|
||
information about that. This is a HISTORICAL SUMMARY, not some "cloak and
|
||
dagger" type junk... What does a "title" matter?
|
||
|
||
BH> It is my opinion this document was written by some college kids
|
||
|
||
That is virtually impossible, considering the sources involved, and those who
|
||
have confirmed it's authenticity. Does AW&ST publish verbatim exerpts from
|
||
something as "phony" as you seem to think it is?
|
||
|
||
BH> There are several gross errors in the parts so far posted.
|
||
|
||
Then by all means pass that on to me in as much DETAIL as possible! I will be
|
||
more than happy to relay it to the Internet and get a response for you.
|
||
|
||
BH> If this were a real CIA document, we would all probably be speaking
|
||
BH> Russian long ago due to their ineptness.
|
||
|
||
That makes ZERO sense as far as i'm concerned. Damn silly thing to say.
|
||
|
||
BH> By the time you have posted the whole thing, I think it will be evident
|
||
BH> to all it is a hoax.
|
||
|
||
Hardly... It seems to contain a VAST amount of explicit detail which does not
|
||
sound anything even remotely close to any "hoax".
|
||
|
||
BH> If there are still some believers left, I will compose a 100%
|
||
BH> genuine placebo message
|
||
|
||
Gee, if you have nothing better to do with your time then feel free. I
|
||
certainly don't have any idea what your point would be though...
|
||
|
||
BH> Author will be Lt.Gen. P.T.Barnum who was CIA Director of USAF affairs.
|
||
|
||
More real funny stuff... What is your problem, anyway?
|
||
|
||
BH> It will say whatever it takes to convince the believers that
|
||
BH> they were taken in.
|
||
|
||
So far all you have "convinced" me of is that you can write a rather obnoxious
|
||
and insulting message, and for no apparent reason. And what does YOUR ability
|
||
to create a "hoax" have to do with ANYTHING?
|
||
|
||
If you want to write something coherent and SERIOUS, I will pass it along to
|
||
those who can reply to it and relay the response back here. But if it's
|
||
-anything- close to what you have written here, then i'm sure they would just
|
||
get a laugh out of it... Since this is a very professional and serious group,
|
||
if all you can write is another flame then it would probably not be appropriate
|
||
for me to even pass it along in the first place.
|
||
|
||
It sounds to me like YOU have been reading too much fiction, since there is
|
||
nothing obviously wrong with this document, and all the facts presented conform
|
||
to the historical references currently available.
|
||
* Origin: SLC-6 Western Spaceport in Simi Valley, CA (1:102/1006.4)
|
||
|
||
Msg#:18735 *AVIATION*
|
||
12/23/91 22:41:00 (Read 0 Times)
|
||
From: DEAN ADAMS
|
||
To: BILL HODGES
|
||
Subj: REPLY TO MSG# 18734 (RE: OX)
|
||
IB >> mailing list on the Internet called Skunk-Works.
|
||
|
||
BH> I'm not familiar with "that".
|
||
|
||
Your loss, but ignorance is no excuse to start a flame campaign.
|
||
|
||
BH> Is it Aviation related? Flying Saucer? Science Fiction? Trekkies?
|
||
|
||
You are really going off the deep end, aren't you? Wow...
|
||
The Internet is a network between Universities, researches, government, and
|
||
technology oriented corporations. Skunk-works is a small net of people
|
||
interested in just what it implies, and participants include
|
||
those from NASA, Lockheed, Boeing, and others.
|
||
|
||
BH> Isn't it strange that no reputable or scandalous radio, TV, Cable, program
|
||
BH> nor newspaper, flyer, scandal sheet, magazine, or book published this
|
||
BH> inside story?
|
||
|
||
I guess you don't like AW&ST then, either.
|
||
|
||
BH> Did anyone try to find the originator of first BBS disclosure
|
||
|
||
YOU are seeing the first "bbs disclosure"!! This is IT! The original paper
|
||
copy was given to someone who helped to restore A-12 (60-6940), with countless
|
||
reputable people involved in the project. He then typed it in a page at a time
|
||
EXACTLY as on the official report, and sent it out to the interested parties
|
||
over the Internet skunk-works mailing list. Just because you are "not familiar"
|
||
with such things, is no reason to start making TOTALLY baseless insults. If
|
||
you have something SERIOUS to say, than by all means lets hear it. Also include
|
||
information about YOU, so those who read it will not just automatically think
|
||
it's just a "hoax" or trouble maker.
|
||
|
||
BH> Does anyone ever consider authentication from a reliable person?
|
||
|
||
I certainly do... And numerous "reliable person's" have said this document
|
||
was authentic. You just seem to be getting wildly carried away with the fact
|
||
it was posted as a "CIA History", and ignoring the great detail and accuracy
|
||
contained after that point... For what reason, I can't imagine. I'm as
|
||
"skeptical" as anyone, but not to the point of being blind to even the clearest
|
||
facts.
|
||
|
||
|