• STRATEGIES FOR A PERMANENT LUNAR BASE 1983

    From Ricky Sutphin@RICKSBBS/TIME to All on Fri Dec 27 15:22:47 2024
    STRATEGIES FOR A PERMANENT LUNAR BASE

    Michael B. Duke, Wendell W. Mendell, and Barney B. Roberts
    NASA-Johnson Space Center, Houston, TX 77058


    Abstract

    Planned activities at a manned lunar base can be categorized as
    supporting one or more of three possible objectives: scientific research, exploration of lunar resources for use in building a space infrastructure,
    or attainment of self-sufficiency in the lunar environment as a first step
    in planetary habitation. Scenarios constructed around each of the three
    goals have many common elements, particularly in the early phases. The
    cost and the complexity of the base, as well as the structure of the Space Transportation System, are functions of the chosen long-term strategy. A
    real lunar base will manifest some combination of characteristics from
    these idealized end members.


    A MOON IN AMERICA'S FUTURE

    The Earth is unique in the solar system, not only for harboring life,
    but also for its relatively massive satellite. It is speculative that the
    two attributes are somehow related, but certainly the Earth's companion
    has left cultural and biological imprints on humanity. As cumulative application of the scientific method has increased our understanding and awareness of the physical universe, fascination with the habitability of
    the Moon has blossomed. As late as the late century, newspaper stories
    reported telescopic observations of the daily lives of lunar creatures.
    The manned lunar landings of the last decade have dispelled such
    romanticism forever but in turn have provided the technology and the information necessary to fulfill a greater dream - the transport of civilization beyond the confines of the Earth.

    Cultural expansion is a recurring theme in human affairs. Motivations
    for exploration or conquest vary from resource limitations (Mongol
    invasions) to religion (Turkish probings of medieval Europe) to commerce (global circumnavigations of the Sixteenth and Seventeenth Centuries).
    American history especially is permeated by the doctrine of manifest
    destiny. The concept of the frontier has come to symbolize for Americans
    the exercise of individual freedom, which in collective expression leads
    to social renewal. Contemporary popular writers cater to this mythos by describing for an overpopulated and confused world the "high frontier" of space. So far, the promise of space has been a reality for a few and only
    a vicarious experience for most. However, humanity, and the United States particularly, stands today at the threshold of a truly new world - the
    Moon.
    ♀ The promise of the Moon is not immediately evident from examination of
    the current American space program. However, the space shuttle and the
    proposed space station can be viewed as building blocks in a general
    purpose space transportation infrastructure (fig. 1). To service
    geosynchronous orbit, an upper stage is needed in addition to the shuttle.
    If that upper stage is provided in the form of a reusable orbit-to-orbit transfer vehicle docked at the space station, the transportation system
    can be multipurpose. In particular, a rudimentary lunar transportation
    system then will exist because the propulsion requirements for attaining geosynchronous orbit and lunar orbit are essentially identical. A lunar
    landing vehicle is required to place payloads on the lunar surface, but
    its design can be a straightforward adaptation of the orbital transfer
    vehicle (OTV). The space station and the reusable OTV constitute a natural evolutionary path that, when achieved, will make accessible all near-Earth space including the Moon. This "enabling technology" is a NASA target for
    the mid 1990's.

    When the requisite technology exists, the American political process inevitably will include lunar surface activities as a major space
    objective. In fact, some sort of declaration may well precede the actual establishment of the space station. It is therefore prudent to consider
    the nature of a permanent manned presence on the Moon and its potential
    impact on the evolution of the Space Transportation System (STS).

    Although the lunar base program is one in which the United States can assert its leadership in space, it is inherently international in scope
    and should involve as much participation as possible from other countries. Opportunities for international cooperation exist in the planning stages,
    in the science and technology development, and in operations at the lunar
    base. A legal framework will be needed to guarantee that potentially profit-making ventures adequately consider the concerns of the
    international community.


    USES OF THE MOON

    A manned lunar base can be discussed in terms of three distinct
    functions. The first involves the scientific investigation of the Moon and
    its environment and the application of special properties of the Moon to research problems. The second produces the capability to utilize the
    materials of the Moon for beneficial purposes throughout the Earth-Moon
    system. The last, and perhaps the most intriguing, is to conduct research
    and development leading to a self-sufficient and self-supporting lunar
    base, the first extraterrestrial human colony. Although these activities
    take place on the Moon, the developed technology and the established
    capability will benefit society on Earth as well as the growing industrialization of near-Earth space.

    Scientific Research
    A lunar base will create new opportunities for investigating the Moon
    and its environment and for using the Moon as a platform for scientific investigations. Analogous to the function of McMurdo Base in Antarctica,
    the lunar base will provide logistical and supporting laboratory
    capability to rapidly expand knowledge of lunar geology, geophysics, environmental science, and resource potential through wide-ranging field investigations, sampling, and placement of instrumentation. Access to
    large, free vacuum volumes may enable new experimental facilities such as macroparticle accelerators. The firm, fixed platform will enable new astronomical interferometric measurements to be obtained (fig. 2). The challenge of long-term, self-sufficient operations on the Moon can spur scientific and technological advances in materials science, bioprocessing, physics and chemistry based on lunar materials, and reprocessing systems.
    These concepts are explored by other papers in this volume.

    ♀Exploitation of Lunar Resources
    It has been argued that major industrialization of space cannot occur without access to the resources of the Moon. Studies of immense projects
    such as solar power satellites have demonstrated that at a sufficiently
    large scale, it is reasonable to develop the resource potential of the
    Moon to offset the high Earth-to-orbit transportation costs (Hearth,
    1976). The lower gravitational field of the Moon and the absence of an atmosphere that retards objects accelerated from the surface provides a potential 20 to 30-fold advantage for launching from the Moon instead of
    Earth. For example, at liftoff, about 1.5% of the space shuttle's mass is payload. Most of the mass is propellant. From the Moon, approximately 50%
    of the mass can be payload.

    The commodity currently envisioned to be most in demand in Earth-Moon
    space over the next three decades is liquid oxygen, which makes up 6/7 of
    the mass of propellant utilized by cryogenic (hydrogen-oxygen) rockets,
    such as the Centaur or postulated OTV's. Although it would appear unlikely
    than an atmosphereless body is a source for oxygen, it is actually an
    abundant element on the Moon (Arnold and Duke, 1978). It must be
    extracted, however, from silicate and oxide minerals into its liquid form
    for use as a propellant. Several processes have been suggested (Criswell,
    1980) for accomplishing this, including reduction of raw soil by fluorine (which is recovered) or reduction or iron-titanium oxide (ilmenite)
    hydrogen (also recovered). Preliminary laboratory studies have verified
    the concepts behind some of these processes.

    Systems studies (e.g., Carrol et al., 1983) show that oxygen
    production on the Moon could benefit STS in the early years of the next century, even if the hydrogen component of the propellant needed to be
    brought from Earth (fig. 3-5). Finding concentrations of water at the
    lunar poles (Arnold, 1979) or extracting the dispersed solar wind-derived hydrogen in the lunar regolith would greatly improve the economics of the transportation system.

    Other commodities also could be produced. Metals, such as iron or
    titanium, can be extracted from the lunar soil or from specific rocks or minerals with differing degrees of difficulty. For example, small
    quantities of metal (primarily iron) from meteorites can be concentrated
    with a magnetic device from large amounts of lunar soil, or, with much
    larger energy inputs, titanium can be obtained from ilmenite. These
    products could find applications in large space structures. Lunar titania
    or alumina might be used to produce aerobrakes (heat shields) used in
    OTV's. In the long term, at relatively high levels of development,
    production of components for solar electric power generation in space
    (e.g., solar power satellites) could be made feasible (Bock, 1979).

    Lunar Autarky
    A self-sufficient lunar base is a possible long-term objective that
    creates new challenges in planning and development. In the near term, emplacement of a controlled environment capsule on the Moon involves known technology. The initial concept for a lunar habitat module is simply an extension of the design experience from Apollo, Skylab, the space shuttle,
    and space station (fig. 6). A different perspective is required to plan
    systems that can utilize the Moon's native materials and energy sources to produce a self-sufficient capability.

    Most of the generic technologies for an advanced system are similar to those employed in general space operations (life support, power, thermal control, communications, logistics, and transportation, etc.), but they
    must be modified to utilize lunar materials for growth and extension. Ultimately, the desire to minimize or to eliminate the resupply link from
    Earth required a host of applications, new to the space program, carried
    to new levels of system reliability. Exploration of technologies such as
    lunar metallurgy, ceramics, manufacturing processes, power systems, and
    others, will reveal whether autarky is a realistic objective and can
    prepare the way for achieving it an operational base. Perhaps this is the
    most compelling rationale for a lunar system, as it promises eventual self-sufficiency elsewhere in the solar system.


    PHASED EVOLUTION OF A LUNAR BASE

    We loosely define three scenarios, each based on one of the long-term rationales described above: scientific research, production, and self-sufficiency (Tables 1-3). Each scenario passes through several
    phases, some of which are common to the other scenarios. The distinction
    among the three views lies with the culminating phase of each.

    Precursor Exploration. Because the scientific data base is incomplete, particularly in the polar regions, the first step in Phase I is global
    mapping of the Moon, both with relatively high resolution imagery and with remote-sensing measurements to determine the chemical variability. This
    task can be accomplished with an unmanned satellite, a Lunar Geochemical Orbiter or LGO (Minear et al., 1977), which is a proposed mission in
    NASA's planetary program and could be flown in the 1990-1992 time frame.
    The LGO is in the Planetary Observer mission class, a low-cost approach to planetary exploration recommended by the report of the Solar System
    Exploration Committee (1983). Secondly, Phase I should include research on technologies necessary to exploit lunar surfaces. Technology development
    in resource problems on Earth is typically a long lead time process. At
    the conclusion of Phase I, the initial site for a base will have been
    defined and planned activities understood in some detail. Concurrently
    with this preliminary phase in the lunar program, development of a space station and on OTV capable of supporting a lunar base would be carried out
    in NASA's STS program.

    Research Output. At Phase II, an initial surface facility would
    establish limited research capability for science, materials processing,
    or lunar surface operations. Depending on the long-term objectives of the
    lunar base program, the detailed studies and the experimental plans start
    to diverge at this phase for the different scenarios. A focus on lunar
    science and astronomy would result in local geological exploration, the establishment of a small astronomical laboratory, and emplacement of
    automated instruments. If production were to be the focus, a pilot plant
    for lunar oxygen extractions could be set up instead, and study of the fabrication of aerobrakes from lunar material could be initiated. If the program goal pointed to achieving self-sufficiency, the emphasis at this
    stage could be agricultural experiments utilizing lunar soil as substrate
    and recycling water, oxygen, and carbon dioxide.

    ♀ To accomplish Phase II in any of the scenarios, the STS must have the capability of landing and taking off from the Moon, transporting manned capsules (about 10,000 kg) to and from the lunar surface, and delivering payloads of about 20,000 kg to the lunar surface. This involves delivering approximately 40,000 kg into lunar orbit using OTV's. The requirement for storage of the return vehicle on the Moon for extended periods (14 days to
    3 months) may require new high-performance, storable propellent systems at
    this phase of development.

    Permanent Occupancy. At Phase III, permanent occupancy is the
    objective. The surface infrastructure would include greater access to
    power, better mobility in and away from the base, and more diversified
    research capability. Still, depending on the long-term objectives, the
    nature of the base can vary. A science base might emphasize long-range traverses for planetological studies or extension of observational
    capability with larger telescopes. A production base will incorporate
    highly automated systems to produce and transfer liquid oxygen for use in
    the transportation system. Advanced research for a self-sufficient base
    would be making first extensions of the base utilizing indigenous
    materials. The production and the self-sufficiency scenarios require a
    small cousin to the Earth-orbit space station in lunar space (lunar orbit
    or an Earth-Moon libration point) to provide for transfer, refueling and maintenance of the lunar lander and the OTV's.

    Advanced Base. The advanced base, Phase IV, is even more specialized. Depending on the long-term plan, it produces more types or a greater range
    of scientific investigations, adds products to the growing lunar
    industrial base, or enters a phase of significant expansion of
    capabilities using lunar materials as the majority of the feedstock. This
    is the terminal phase for the science and production scenarios. Future
    growth may occur by enlarging the number of experiments or products
    produced on the Moon, but a self-sustaining capability is not included.
    The production base might even develop toward a highly automated state
    where permanent occupancy was unnecessary. For the production and
    independence scenarios, the base should begin paying its own operational
    costs. In the self-sufficiency scenario, research and development of pilot plants aimed at a broad range of indigenous ;lunar technologies would be pursued. The final phase of the self-sufficiency scenario is a truly
    autarkic settlement, a lunar colony, in which the link to Earth can be discretionary.

    EVOLUTION OF THE PROGRAM

    Figure 7 ties the possible development of a lunar base to the growth
    of lunar resource support of the transportation system. Initially, the
    base is totally dependent on terrestrial supply where 7 kg in low-Earth
    orbit is required to place 1 kg on the lunar surface. With the
    introduction of lunar oxygen first into near-Moon operations and then into
    the return leg of the transportation system, the slope of the curve
    changes from 7:1 to 3.5:1. As the lunar manufacturing capability increases
    to the point where aerobrakes can be manufactured, the slope decreases to somewhat slightly greater than 1:1. Further growth of lunar capability
    allows expansion of base mass to be more or less independent of the
    quantity of imported terrestrial mass. At the point of self-sufficiency,
    only trace minerals and crew changeout are chargeable weight to lunar operations; the slope of the curve in fig. 7 is essentially flat.

    Another consideration in the growth of lunar activities is the
    economic "balance of trade" between Earth orbit and the lunar surface. The value of lunar products may support lunar operations before a true mass
    balance is achieved. It is difficult to calculate the economic value of
    lunar oxygen and other products in low-Earth orbit. However these "lunar credits" are shown qualitatively in fig. 7 at the point where a closed ecological life support system (CELSS) and a significant manufacturing capability are available. The slope of the "credits" line will be a
    function of many things, such as the amount of oxygen required to support non-lunar activities, the value of science and research enabled by the
    lunar base. Finally, the dashed line of constant slope indicates the
    continued total dependency that would exist if these technologies are not pursued on the Moon, that is, if a self-sufficiency element is not
    included in the lunar base program.

    The real lunar base will evolve as some combination of the above
    scenarios. Determination of the right mix requires research, development,
    and debate. Even if a program is started now, several years should be
    devoted to study of the detailed lunar base scenario. The time is
    available because the development of the space transportation
    infrastructure and the completion of the orbital science survey will take
    7-10 years. Proper preparation will make it possible to decide on a
    specific lunar base design in the early 1990's. That time frame is
    consistent with the development of the infrastructure that will enable the lunar base program to be carried out to its full potential. The first
    manned landings could occur early in the first decade of the next century; permanent occupancy could be achieved by the year 2007, the fiftieth anniversary of the Space Age.

    There are potential technological problems that may slow the
    development of the lunar base, and at each phase there will be serious questions as to whether to proceed and how and when to proceed. A
    commitment need not be made now to the whole plan. Nevertheless, the
    long-term objective is one of immense significance in human history and
    should not be casually discarded. It is inevitable that humankind will
    settle the Moon and other bodies in the Solar System. We live in a
    generation that has already taken very significant steps along that path.
    With careful planning, we can nuture the capability to move from the
    planet, to provide benefits to Earth, and to satisfy humanity's spirit of adventure.

    REFERENCES

    Arnold, James R. (1979) Ice in the lunar polar regions, J. Geophys.
    Res., 84, 5659-5668.

    Arnold, James R. and Duke, Michael B. (1978) Summer Workshop On
    Near-Earth Resources, NASA CP-2031, NASA, Washington, DC, 1-7 pp.

    Bock, Edward H. (1979) Lunar Resources Utilization for Space
    Construction, Final Report for Contract NAS9-15560, General Dynamics
    Convair Div., Advanced Space Programs, San Diego, CA.

    Carroll, W. F., Steurer, W. H., Frisbee, R. H., and Jones, R. M.
    (1983) Extraterrestrial materials - Their role in future space
    operations, Astronaut, Aeronaut, 21, 80-85.

    Criswell, David R. (1980) Extraterrestrial materials processing and
    construction, Final Report Contr. NSR 09-051-001, Lunar and Planetary
    Institute, Houston, TX.

    ♀Hearth, Donald P. (1976) Outlook for Space, NASA SP-386, NASA, Wash., DC,
    237 pp.

    Minear, J. W., Hubbard, N., Johnson, T.V., and Clarke, V. C., Jr. (1977) Mission Summary for Lunar Polar Orbiter, JPL Document 660-41, Rev. A., Jet Propulsion Laboratory, Pasadena, CA.,36 pp

    Solar System Exploration Committee (1983) Planetary Exploration Through
    Year 2000: A Core Program, U.S. Government Printing Office, Washington,
    DC, 167 pp.

    Figure Titles

    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

    ♀→

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