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27 KiB
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507 lines
27 KiB
Plaintext
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STRATEGIES FOR A PERMANENT LUNAR BASE
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Michael B. Duke, Wendell W. Mendell, and Barney B. Roberts
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NASA-Johnson Space Center, Houston, TX 77058
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Abstract
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Planned activities at a manned lunar base can be categorized as
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supporting one or more of three possible objectives: scientific research,
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exploration of lunar resources for use in building a space infrastructure,
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or attainment of self-sufficiency in the lunar environment as a first step
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in planetary habitation. Scenarios constructed around each of the three
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goals have many common elements, particularly in the early phases. The
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cost and the complexity of the base, as well as the structure of the Space
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Transportation System, are functions of the chosen long-term strategy. A
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real lunar base will manifest some combination of characteristics from
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these idealized end members.
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A MOON IN AMERICA'S FUTURE
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The Earth is unique in the solar system, not only for harboring life,
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but also for its relatively massive satellite. It is speculative that the
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two attributes are somehow related, but certainly the Earth's companion
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has left cultural and biological imprints on humanity. As cumulative
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application of the scientific method has increased our understanding and
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awareness of the physical universe, fascination with the habitability of
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the Moon has blossomed. As late as the late century, newspaper stories
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reported telescopic observations of the daily lives of lunar creatures.
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The manned lunar landings of the last decade have dispelled such
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romanticism forever but in turn have provided the technology and the
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information necessary to fulfill a greater dream - the transport of
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civilization beyond the confines of the Earth.
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Cultural expansion is a recurring theme in human affairs. Motivations
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for exploration or conquest vary from resource limitations (Mongol
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invasions) to religion (Turkish probings of medieval Europe) to commerce
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(global circumnavigations of the Sixteenth and Seventeenth Centuries).
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American history especially is permeated by the doctrine of manifest
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destiny. The concept of the frontier has come to symbolize for Americans
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the exercise of individual freedom, which in collective expression leads
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to social renewal. Contemporary popular writers cater to this mythos by
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describing for an overpopulated and confused world the "high frontier" of
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space. So far, the promise of space has been a reality for a few and only
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a vicarious experience for most. However, humanity, and the United States
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particularly, stands today at the threshold of a truly new world - the
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Moon.
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The promise of the Moon is not immediately evident from examination of
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the current American space program. However, the space shuttle and the
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proposed space station can be viewed as building blocks in a general
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purpose space transportation infrastructure (fig. 1). To service
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geosynchronous orbit, an upper stage is needed in addition to the shuttle.
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If that upper stage is provided in the form of a reusable orbit-to-orbit
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transfer vehicle docked at the space station, the transportation system
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can be multipurpose. In particular, a rudimentary lunar transportation
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system then will exist because the propulsion requirements for attaining
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geosynchronous orbit and lunar orbit are essentially identical. A lunar
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landing vehicle is required to place payloads on the lunar surface, but
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its design can be a straightforward adaptation of the orbital transfer
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vehicle (OTV). The space station and the reusable OTV constitute a natural
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evolutionary path that, when achieved, will make accessible all near-Earth
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space including the Moon. This "enabling technology" is a NASA target for
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the mid 1990's.
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When the requisite technology exists, the American political process
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inevitably will include lunar surface activities as a major space
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objective. In fact, some sort of declaration may well precede the actual
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establishment of the space station. It is therefore prudent to consider
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the nature of a permanent manned presence on the Moon and its potential
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impact on the evolution of the Space Transportation System (STS).
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Although the lunar base program is one in which the United States can
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assert its leadership in space, it is inherently international in scope
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and should involve as much participation as possible from other countries.
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Opportunities for international cooperation exist in the planning stages,
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in the science and technology development, and in operations at the lunar
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base. A legal framework will be needed to guarantee that potentially
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profit-making ventures adequately consider the concerns of the
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international community.
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USES OF THE MOON
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A manned lunar base can be discussed in terms of three distinct
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functions. The first involves the scientific investigation of the Moon and
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its environment and the application of special properties of the Moon to
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research problems. The second produces the capability to utilize the
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materials of the Moon for beneficial purposes throughout the Earth-Moon
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system. The last, and perhaps the most intriguing, is to conduct research
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and development leading to a self-sufficient and self-supporting lunar
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base, the first extraterrestrial human colony. Although these activities
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take place on the Moon, the developed technology and the established
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capability will benefit society on Earth as well as the growing
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industrialization of near-Earth space.
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Scientific Research
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A lunar base will create new opportunities for investigating the Moon
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and its environment and for using the Moon as a platform for scientific
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investigations. Analogous to the function of McMurdo Base in Antarctica,
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the lunar base will provide logistical and supporting laboratory
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capability to rapidly expand knowledge of lunar geology, geophysics,
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environmental science, and resource potential through wide-ranging field
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investigations, sampling, and placement of instrumentation. Access to
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large, free vacuum volumes may enable new experimental facilities such as
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macroparticle accelerators. The firm, fixed platform will enable new
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astronomical interferometric measurements to be obtained (fig. 2). The
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challenge of long-term, self-sufficient operations on the Moon can spur
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scientific and technological advances in materials science, bioprocessing,
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physics and chemistry based on lunar materials, and reprocessing systems.
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These concepts are explored by other papers in this volume.
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Exploitation of Lunar Resources
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It has been argued that major industrialization of space cannot occur
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without access to the resources of the Moon. Studies of immense projects
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such as solar power satellites have demonstrated that at a sufficiently
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large scale, it is reasonable to develop the resource potential of the
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Moon to offset the high Earth-to-orbit transportation costs (Hearth,
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1976). The lower gravitational field of the Moon and the absence of an
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atmosphere that retards objects accelerated from the surface provides a
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potential 20 to 30-fold advantage for launching from the Moon instead of
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Earth. For example, at liftoff, about 1.5% of the space shuttle's mass is
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payload. Most of the mass is propellant. From the Moon, approximately 50%
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of the mass can be payload.
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The commodity currently envisioned to be most in demand in Earth-Moon
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space over the next three decades is liquid oxygen, which makes up 6/7 of
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the mass of propellant utilized by cryogenic (hydrogen-oxygen) rockets,
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such as the Centaur or postulated OTV's. Although it would appear unlikely
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than an atmosphereless body is a source for oxygen, it is actually an
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abundant element on the Moon (Arnold and Duke, 1978). It must be
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extracted, however, from silicate and oxide minerals into its liquid form
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for use as a propellant. Several processes have been suggested (Criswell,
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1980) for accomplishing this, including reduction of raw soil by fluorine
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(which is recovered) or reduction or iron-titanium oxide (ilmenite)
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hydrogen (also recovered). Preliminary laboratory studies have verified
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the concepts behind some of these processes.
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Systems studies (e.g., Carrol et al., 1983) show that oxygen
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production on the Moon could benefit STS in the early years of the next
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century, even if the hydrogen component of the propellant needed to be
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brought from Earth (fig. 3-5). Finding concentrations of water at the
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lunar poles (Arnold, 1979) or extracting the dispersed solar wind-derived
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hydrogen in the lunar regolith would greatly improve the economics of the
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transportation system.
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Other commodities also could be produced. Metals, such as iron or
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titanium, can be extracted from the lunar soil or from specific rocks or
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minerals with differing degrees of difficulty. For example, small
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quantities of metal (primarily iron) from meteorites can be concentrated
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with a magnetic device from large amounts of lunar soil, or, with much
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larger energy inputs, titanium can be obtained from ilmenite. These
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products could find applications in large space structures. Lunar titania
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or alumina might be used to produce aerobrakes (heat shields) used in
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OTV's. In the long term, at relatively high levels of development,
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production of components for solar electric power generation in space
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(e.g., solar power satellites) could be made feasible (Bock, 1979).
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Lunar Autarky
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A self-sufficient lunar base is a possible long-term objective that
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creates new challenges in planning and development. In the near term,
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emplacement of a controlled environment capsule on the Moon involves known
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technology. The initial concept for a lunar habitat module is simply an
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extension of the design experience from Apollo, Skylab, the space shuttle,
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and space station (fig. 6). A different perspective is required to plan
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systems that can utilize the Moon's native materials and energy sources to
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produce a self-sufficient capability.
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Most of the generic technologies for an advanced system are similar to
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those employed in general space operations (life support, power, thermal
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control, communications, logistics, and transportation, etc.), but they
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must be modified to utilize lunar materials for growth and extension.
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Ultimately, the desire to minimize or to eliminate the resupply link from
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Earth required a host of applications, new to the space program, carried
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to new levels of system reliability. Exploration of technologies such as
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lunar metallurgy, ceramics, manufacturing processes, power systems, and
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others, will reveal whether autarky is a realistic objective and can
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prepare the way for achieving it an operational base. Perhaps this is the
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most compelling rationale for a lunar system, as it promises eventual
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self-sufficiency elsewhere in the solar system.
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PHASED EVOLUTION OF A LUNAR BASE
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We loosely define three scenarios, each based on one of the long-term
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rationales described above: scientific research, production, and
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self-sufficiency (Tables 1-3). Each scenario passes through several
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phases, some of which are common to the other scenarios. The distinction
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among the three views lies with the culminating phase of each.
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Precursor Exploration. Because the scientific data base is incomplete,
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particularly in the polar regions, the first step in Phase I is global
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mapping of the Moon, both with relatively high resolution imagery and with
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remote-sensing measurements to determine the chemical variability. This
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task can be accomplished with an unmanned satellite, a Lunar Geochemical
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Orbiter or LGO (Minear et al., 1977), which is a proposed mission in
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NASA's planetary program and could be flown in the 1990-1992 time frame.
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The LGO is in the Planetary Observer mission class, a low-cost approach to
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planetary exploration recommended by the report of the Solar System
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Exploration Committee (1983). Secondly, Phase I should include research on
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technologies necessary to exploit lunar surfaces. Technology development
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in resource problems on Earth is typically a long lead time process. At
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the conclusion of Phase I, the initial site for a base will have been
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defined and planned activities understood in some detail. Concurrently
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with this preliminary phase in the lunar program, development of a space
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station and on OTV capable of supporting a lunar base would be carried out
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in NASA's STS program.
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Research Output. At Phase II, an initial surface facility would
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establish limited research capability for science, materials processing,
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or lunar surface operations. Depending on the long-term objectives of the
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lunar base program, the detailed studies and the experimental plans start
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to diverge at this phase for the different scenarios. A focus on lunar
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science and astronomy would result in local geological exploration, the
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establishment of a small astronomical laboratory, and emplacement of
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automated instruments. If production were to be the focus, a pilot plant
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for lunar oxygen extractions could be set up instead, and study of the
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fabrication of aerobrakes from lunar material could be initiated. If the
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program goal pointed to achieving self-sufficiency, the emphasis at this
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stage could be agricultural experiments utilizing lunar soil as substrate
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and recycling water, oxygen, and carbon dioxide.
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To accomplish Phase II in any of the scenarios, the STS must have the
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capability of landing and taking off from the Moon, transporting manned
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capsules (about 10,000 kg) to and from the lunar surface, and delivering
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payloads of about 20,000 kg to the lunar surface. This involves delivering
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approximately 40,000 kg into lunar orbit using OTV's. The requirement for
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storage of the return vehicle on the Moon for extended periods (14 days to
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3 months) may require new high-performance, storable propellent systems at
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this phase of development.
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Permanent Occupancy. At Phase III, permanent occupancy is the
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objective. The surface infrastructure would include greater access to
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power, better mobility in and away from the base, and more diversified
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research capability. Still, depending on the long-term objectives, the
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nature of the base can vary. A science base might emphasize long-range
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traverses for planetological studies or extension of observational
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capability with larger telescopes. A production base will incorporate
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highly automated systems to produce and transfer liquid oxygen for use in
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the transportation system. Advanced research for a self-sufficient base
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would be making first extensions of the base utilizing indigenous
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materials. The production and the self-sufficiency scenarios require a
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small cousin to the Earth-orbit space station in lunar space (lunar orbit
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or an Earth-Moon libration point) to provide for transfer, refueling and
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maintenance of the lunar lander and the OTV's.
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Advanced Base. The advanced base, Phase IV, is even more specialized.
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Depending on the long-term plan, it produces more types or a greater range
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of scientific investigations, adds products to the growing lunar
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industrial base, or enters a phase of significant expansion of
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capabilities using lunar materials as the majority of the feedstock. This
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is the terminal phase for the science and production scenarios. Future
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growth may occur by enlarging the number of experiments or products
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produced on the Moon, but a self-sustaining capability is not included.
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The production base might even develop toward a highly automated state
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where permanent occupancy was unnecessary. For the production and
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independence scenarios, the base should begin paying its own operational
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costs. In the self-sufficiency scenario, research and development of pilot
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plants aimed at a broad range of indigenous ;lunar technologies would be
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pursued. The final phase of the self-sufficiency scenario is a truly
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autarkic settlement, a lunar colony, in which the link to Earth can be
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discretionary.
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EVOLUTION OF THE PROGRAM
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Figure 7 ties the possible development of a lunar base to the growth
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of lunar resource support of the transportation system. Initially, the
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base is totally dependent on terrestrial supply where 7 kg in low-Earth
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orbit is required to place 1 kg on the lunar surface. With the
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introduction of lunar oxygen first into near-Moon operations and then into
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the return leg of the transportation system, the slope of the curve
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changes from 7:1 to 3.5:1. As the lunar manufacturing capability increases
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to the point where aerobrakes can be manufactured, the slope decreases to
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somewhat slightly greater than 1:1. Further growth of lunar capability
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allows expansion of base mass to be more or less independent of the
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quantity of imported terrestrial mass. At the point of self-sufficiency,
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only trace minerals and crew changeout are chargeable weight to lunar
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operations; the slope of the curve in fig. 7 is essentially flat.
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Another consideration in the growth of lunar activities is the
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economic "balance of trade" between Earth orbit and the lunar surface. The
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value of lunar products may support lunar operations before a true mass
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balance is achieved. It is difficult to calculate the economic value of
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lunar oxygen and other products in low-Earth orbit. However these "lunar
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credits" are shown qualitatively in fig. 7 at the point where a closed
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ecological life support system (CELSS) and a significant manufacturing
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capability are available. The slope of the "credits" line will be a
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function of many things, such as the amount of oxygen required to support
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non-lunar activities, the value of science and research enabled by the
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lunar base. Finally, the dashed line of constant slope indicates the
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continued total dependency that would exist if these technologies are not
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pursued on the Moon, that is, if a self-sufficiency element is not
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included in the lunar base program.
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The real lunar base will evolve as some combination of the above
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scenarios. Determination of the right mix requires research, development,
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and debate. Even if a program is started now, several years should be
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devoted to study of the detailed lunar base scenario. The time is
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available because the development of the space transportation
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infrastructure and the completion of the orbital science survey will take
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7-10 years. Proper preparation will make it possible to decide on a
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specific lunar base design in the early 1990's. That time frame is
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consistent with the development of the infrastructure that will enable the
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lunar base program to be carried out to its full potential. The first
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manned landings could occur early in the first decade of the next century;
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permanent occupancy could be achieved by the year 2007, the fiftieth
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anniversary of the Space Age.
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There are potential technological problems that may slow the
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development of the lunar base, and at each phase there will be serious
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questions as to whether to proceed and how and when to proceed. A
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commitment need not be made now to the whole plan. Nevertheless, the
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long-term objective is one of immense significance in human history and
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should not be casually discarded. It is inevitable that humankind will
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settle the Moon and other bodies in the Solar System. We live in a
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generation that has already taken very significant steps along that path.
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With careful planning, we can nuture the capability to move from the
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planet, to provide benefits to Earth, and to satisfy humanity's spirit of
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adventure.
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REFERENCES
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Arnold, James R. (1979) Ice in the lunar polar regions, J. Geophys.
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Res., 84, 5659-5668.
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Arnold, James R. and Duke, Michael B. (1978) Summer Workshop On
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Near-Earth Resources, NASA CP-2031, NASA, Washington, DC, 1-7 pp.
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Bock, Edward H. (1979) Lunar Resources Utilization for Space
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Construction, Final Report for Contract NAS9-15560, General Dynamics
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Convair Div., Advanced Space Programs, San Diego, CA.
|
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Carroll, W. F., Steurer, W. H., Frisbee, R. H., and Jones, R. M.
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|
(1983) Extraterrestrial materials - Their role in future space
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|
operations, Astronaut, Aeronaut, 21, 80-85.
|
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Criswell, David R. (1980) Extraterrestrial materials processing and
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|
construction, Final Report Contr. NSR 09-051-001, Lunar and Planetary
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|
Institute, Houston, TX.
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|
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Hearth, Donald P. (1976) Outlook for Space, NASA SP-386, NASA, Wash., DC,
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237 pp.
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Minear, J. W., Hubbard, N., Johnson, T.V., and Clarke, V. C., Jr. (1977)
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Mission Summary for Lunar Polar Orbiter, JPL Document 660-41, Rev. A., Jet
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|
Propulsion Laboratory, Pasadena, CA.,36 pp
|
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|
|
|||
|
Solar System Exploration Committee (1983) Planetary Exploration Through
|
|||
|
Year 2000: A Core Program, U.S. Government Printing Office, Washington,
|
|||
|
DC, 167 pp.
|
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|
|
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|
Figure Titles
|
|||
|
|
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|
Figure 1. The Space Transportation System of the future may service a
|
|||
|
station in geosynchronous orbit as well as a lunar base via a station in
|
|||
|
lunar space. The lift capacity of the Shuttle fleet may be augmented by an
|
|||
|
unmanned heavy lift vehicle, designed to ship fuel and consumables to
|
|||
|
space.
|
|||
|
|
|||
|
Figure 2. A radio telescope located on the farside of the Moon would be
|
|||
|
shielded from background noises generated by terrestrial sources. Although
|
|||
|
depicted here with a parabolic dish in a convenient crater, an initial
|
|||
|
lunar instrument may well be a phased array of dipole antennas.
|
|||
|
|
|||
|
Figure 3. Liquid oxygen fuel (LOX), manufactured on the Moon and delivered
|
|||
|
to low-Earth orbit may become a profitable export for a lunar base. A
|
|||
|
critical parameter in analyses of the system is the mass payback ratio,
|
|||
|
defined as the ratio of the excess lunar LOX in LEO to the liquid hydrogen
|
|||
|
fuel delivered from Earth to LEO.
|
|||
|
|
|||
|
Figure 4. The mass payback ratio for lunar LOX delivered to LEO is
|
|||
|
sensitive to the design characteristics of the OTV used as a lunar
|
|||
|
freighter. The fractional mass of the OTV aerobrake and the oxidizer to
|
|||
|
fuel ratio are key parameters. Manufacture of aerobrakes on the Moon would
|
|||
|
enhance system performance.
|
|||
|
|
|||
|
Figure 5. A simple cost-benefit analysis assumes that a lunar oxygen
|
|||
|
production facility has its capital costs amortized solely by "profits" on
|
|||
|
delivery of LOX to LEO. While lunar oxygen is competitive with shuttle
|
|||
|
delivery in all cases, introduction of a cost-efficient heavy lift vehicle
|
|||
|
reduces the advantage under more conservative cost estimates for the lunar
|
|||
|
operation. If costs of lunar LOX are shared with other activities, the
|
|||
|
advantage is restored.
|
|||
|
|
|||
|
Figure 6. The first lunar base habitats and laboratories could be space
|
|||
|
station modules, buried in the lunar regolith for protection from solar
|
|||
|
flare radiation. Interface modules not only interconnect the buries
|
|||
|
structures but also can be stacked to create exits to the surface.
|
|||
|
|
|||
|
Figure 7. Initially, almost 7 kg must be lifted into LEO for every kg
|
|||
|
landed on the Moon. As lunar oxygen is introduced into the transportation
|
|||
|
system, the ratio improves as a unit mass goes from Earth to Moon with
|
|||
|
only little overhead in the system. In a Phase IV advanced base, the
|
|||
|
growth of lunar surface infrastructure becomes only weakly dependent on
|
|||
|
imports from Earth. A favorable balance of trade is ultimately
|
|||
|
conceivable.
|
|||
|
|
|||
|
Table 1. Lunar Base Growth Phases: Sciences Base Scenario
|
|||
|
|
|||
|
A growing capability to do lunar science and to use the Moon as a research
|
|||
|
base for other disciplines, using lunar resources to a limited extent to
|
|||
|
support operations.
|
|||
|
Phase I: Preparatory exploration
|
|||
|
. Lunar orbiter explorer and mapper
|
|||
|
. Instrument and experiment definition
|
|||
|
. Site selection
|
|||
|
. Automated site preparation
|
|||
|
|
|||
|
Phase II: Research Outpost
|
|||
|
. Minimum base, temporarily occupied, totally resupplied from Earth
|
|||
|
. Small telescope/Geoscience module
|
|||
|
. Short range science sorties
|
|||
|
. Instrument package emplacement
|
|||
|
|
|||
|
Phase III: Operational Base
|
|||
|
. Permanently occupied facility
|
|||
|
. Consumable production/Recycling pilot plant
|
|||
|
. Longer range science sorties
|
|||
|
. Geoscience/Biomedical laboratory
|
|||
|
. Experimental lunar telescope
|
|||
|
. Extended surface science experimental packages
|
|||
|
|
|||
|
Phase IV: Advanced Base
|
|||
|
. Advanced consumable production
|
|||
|
. Satellite outposts
|
|||
|
. Advanced geoscience laboratory
|
|||
|
. Plant research laboratory
|
|||
|
. Advanced astronomical observatory
|
|||
|
. Long-range surface exploration
|
|||
|
|
|||
|
|
|||
|
Table 2. Lunar Base Growth Phases Production Base Scenario
|
|||
|
|
|||
|
A lunar base that is intended to develop one or more products for
|
|||
|
commercial use. Manned activity may be continuous, but a high degree of
|
|||
|
automation is expected.
|
|||
|
|
|||
|
Phase I: Preparatory exploration
|
|||
|
. Lunar orbiter explorer and mapper
|
|||
|
. Lunar pilot plant definition
|
|||
|
. Site selection
|
|||
|
. Automated site preparation
|
|||
|
|
|||
|
Phase II: Research outpost
|
|||
|
. Minimum base, temporarily occupied, totally resupplied from Earth
|
|||
|
. Surface mining pilot operation
|
|||
|
. Lunar oxygen pilot plant
|
|||
|
. Lunar materials utilization research module
|
|||
|
|
|||
|
Phase III: Operational base
|
|||
|
. Permanently occupied base
|
|||
|
. Expanded mining facility
|
|||
|
. Consumables supplied locally
|
|||
|
. Oxygen production plant
|
|||
|
. Lunar materials processing pilot plant(s)
|
|||
|
|
|||
|
Phase IV: Advanced base
|
|||
|
. Large scale oxygen production
|
|||
|
. Ceramics/Metals production facility
|
|||
|
. Locally derived consumables for industrial use
|
|||
|
. Industrial research facility
|
|||
|
|
|||
|
|
|||
|
Table 3. Lunar Growth Phases: Lunar Self-Sufficiency Research Base
|
|||
|
Scenario
|
|||
|
|
|||
|
A lunar base that grows in its capacity to support itself and expand its
|
|||
|
capabilities utilizing the indigenous resources of the Moon, with the
|
|||
|
ultimate objective of becoming independent of Earth.
|
|||
|
|
|||
|
Phase I: Preparatory exploration
|
|||
|
. Lunar orbiter explorer and mapper
|
|||
|
. Process definition
|
|||
|
. Site selection
|
|||
|
. Automated site preparation
|
|||
|
|
|||
|
Phase II: Research Outpost
|
|||
|
. Minimum base, temporarily occupied, totally resupplied from Earth
|
|||
|
. Surface mining, pilot operation
|
|||
|
. Lunar oxygen production pilot plant
|
|||
|
. Closed systems research module
|
|||
|
|
|||
|
Phase III: Operational base
|
|||
|
. Permanently occupied facility
|
|||
|
. Expanded mining facility
|
|||
|
. Lunar agriculture research laboratory
|
|||
|
. Lunar materials processing pilot plant(s)
|
|||
|
|
|||
|
Phase IV: Advanced base
|
|||
|
. Lunar ecology research laboratory
|
|||
|
. Lunar power station-90% lunar materials-derived
|
|||
|
. Agriculture production pilot plant
|
|||
|
. Lunar manufacturing facility
|
|||
|
. Oxygen production plant
|
|||
|
. Lunar volatile extraction pilot plant
|
|||
|
|
|||
|
Phase V: Self-sufficient colony
|
|||
|
. Full-scale production of exportable oxygen
|
|||
|
. Volatile production for agriculture, Moon-orbit transportation
|
|||
|
. Closed ecological life support system
|
|||
|
. Lunar manufacturing facility: tools, containment systems, fabricated
|
|||
|
assemblies. etc.
|
|||
|
. Lunar power station - 100% lunar materials - derived
|
|||
|
. Expanding population base
|
|||
|
|
|||
|
|