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Space vehicles -- Auxiliary power supply

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• Space vehicles

• Space vehicles -- Auxiliary power supply -- Analyses
• Space vehicles -- Auxiliary power supply -- Automatic control
• Space vehicles -- Auxiliary power supply -- Automation
• Space vehicles -- Auxiliary power supply -- Brayton cycle
• Space vehicles -- Auxiliary power supply -- Congresses
• Space vehicles -- Auxiliary power supply -- Cooling
• Space vehicles -- Auxiliary power supply -- Design and construction
• Space vehicles -- Auxiliary power supply -- Equipment and supplies
• Space vehicles -- Auxiliary power supply -- Materials
• Space vehicles -- Auxiliary power supply -- Mathematical models
• Space vehicles -- Auxiliary power supply -- Rankine cycle
• Space vehicles -- Auxiliary power supply -- Research
• Space vehicles -- Auxiliary power supply -- Safety measures
• Space vehicles -- Auxiliary power supply -- Testing
• Project SNAP
• Space vehicles -- Batteries
• Space vehicles -- Electric equipment
• Space vehicles -- Solar engines

• Space power-plants

• Development of a Hydrogen-Oxygen Internal Combustion Engine Auxiliary Electric Power Supply System (Detroit and Torrance, CA: Vickers Incorporated Division, Sperry Rand Corp., Aerospace Division, 1963), by Norman Evan Morgan (page images at HathiTrust)
• Design of space powerplants. (Prentice-Hall, 1963), by Donald Bawden Mackay (page images at HathiTrust)
• Flying reactors : the political feasibility of nuclear power in space (Air University Press, 2005), by James R. Downey and Research Air University (U.S.). Center for Aerospace Doctrine (page images at HathiTrust)
• Safety analysis report : SNAPTRAN 2/10A-3 water immersion tests (U.S. Atomic Energy Commission, Idaho Operations Office, 1964), by F. L. Bentzen, J. M. Waage, Idaho National Reactor Testing Station, and Phillips Petroleum Company. Atomic Energy Division (page images at HathiTrust)
• Forced-flow once-through boilers : NASA research (Scientific and Technical Information Office, National Aeronautics and Space Administration ;, 1975), by James R. Stone, Vernon H Gray, Orlando A Gutierrez, and Lewis Research Center (page images at HathiTrust)
• Power sources for deep space probes (The Office, 1998), by United States General Accounting Office (page images at HathiTrust)
• Spacecraft power (National Aeronautics and Space Administration; [for sale by the Supt. of Docs., U.S. Govt. Print. Off., 1970), by William R. Corliss (page images at HathiTrust)
• Digital computer study of nuclear reactor thermal transients during startup of 60-kWe Brayton power conversion system (National Aeronautics and Space Administration ;, 1974), by Kent S. Jefferies, Roy C. Tew, and Lewis Research Center (page images at HathiTrust)
• Concept report : microprocessor control of electric power system (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), by Eugene Perry and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Effects of vibration and shock on the performance of gas-bearing space power Brayton cycle turbomachinery. I, Half-sine shock and sinusoidal vibration (National Aeronautics and Space Administration ;, 1971), by Paul R. Spencer, Henry B. Tryon, Peter W. Curwen, and Mechanical Technology Incorporated (page images at HathiTrust)
• Heat and momentum transfer model studies applicable to once-through, forced convection potassium boiling (National Aeronautics and Space Administration ;, 1971), by C. M. Sabin, Heinz Frank Poppendiek, Lewis Research Center, and Geoscience Consulting Ltd (page images at HathiTrust)
• Deployable space solar power supply (National Aeronautics and Space Administration, 1964), by H. U. Schuerch, W. Robbins, Astro Research Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Development of a thermionic diode controlled power system (National Aeronautics and Space Administration ;, 1966), by H. Dean Venable, Goddard Space Flight Center, Fairchild Hiller Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Development of a hydrogen-oxygen internal combustion engine space power system (For sale by the Clearinghouse for Federal Scientific and Technical Information, 1965), by Norman Evan Morgan, W. D. Morath, United States National Aeronautics and Space Administration, and Incorporated Vickers (page images at HathiTrust)
• Stabilization of carbon and nitrogen in stainless steel and its effect on mass transfer in a stainless steel - Cb-1Zr - potassium system / R. W. Harrison. (National Aeronautics and Space Administration, 1967), by R. W. Harrison (page images at HathiTrust; US access only)
• A study of the feasibility of directly applying gas generator systems to space shuttle mechanical functions (National Aeronautics and Space Administration ;, 1974), by E. Raymond Lake, Langley Research Center, and McDonnell Aircraft Company (page images at HathiTrust)
• University role in astronaut life support systems : space power supply systems (National Aeronautics and Space Administration ;, 1972), by Lang Y. Chin, United States National Aeronautics and Space Administration, and Massachusetts Institute of Technology (page images at HathiTrust)
• High-performance "once-through" boiling of potassium in single tubes at saturation temperatures of 1500⁰ to 1750⁰ F (National Aeronautics and Space Administration, 1967), by J. R. Peterson (page images at HathiTrust; US access only)
• Vaporization of high-temperature potassium in forced convection at saturation temperatures of 1800⁰ to 2100⁰ F (National Aeronautics and Space Administration, 1967), by J. A. Bond and G. L. Converse (page images at HathiTrust; US access only)
• Lunar dust transport and potential interactions with power system components (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), by Cynthia M. Katzan, Jonathan L. Edwards, Inc Sverdrup Technology, and Lewis Research Center (page images at HathiTrust)
• NASA TN D-4532 (National Aeronautics and Space Administration ;, 1968), by John M. Jerke, Atwood R. Heath, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-4407 (National Aeronautics and Space Administration ;, 1968), by Gilbert A. Haynes, Walter E. Ellis, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Current from a dilute plasma measured through holes in insulators (National Aeronautics and Space Administration ;, 1975), by Norman T. Grier, Stanley Domitz, and Lewis Research Center (page images at HathiTrust)
• NASA TN D-5752 (National Aeronautics and Space Administration :, 1970), by Frederick T. Schuller, William J. Anderson, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• A nickel-cadmium battery reconditioning circuit (National Aeronautics and Space Administration ;, 1977), by Roy Lanier and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Transport dynamics of a high-power-density matrix-type hydrogen-oxygen fuel cell (National Aeronautics and Space Administration ;, 1974), by Paul R. Prokopius, Norman H. Hagedorn, and Lewis Research Center (page images at HathiTrust)
• NASA TN D-4727 (National Aeronautics and Space Administration ;, 1968), by William J. Bifano, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Predictability of Brayton electric power system performance (National Aeronautics and Space Administration ;, 1972), by John L. Klann, Henry J. Hettel, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Apollo experience report : the cryogenic storage system (National Aeronautics and Space Administration ;, 1973), by William A. Chandler, Robert K. Allgeier, Robert R. Rice, and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
• Description and simulation of an integrated power and attitude control system concept for space-vehicle application (National Aeronautics and Space Administration ;, 1974), by Ralph W. Will, Kenneth L. Jacobs, Claude R. Keckler, and Langley Research Center (page images at HathiTrust)
• Development of an air flow thermal balance calorimeter (National Aeronautics and Space Administration ;, 1972), by Joseph M. Sherfey, United States National Aeronautics and Space Administration, and Goddard Space Flight Center (page images at HathiTrust)
• Experimental nozzle expansion and flow characteristics of potassium vapor (National Aeronautics and Space Administration ;, 1966), by Louis J. Goldman, Stanley M. Nosek, and Lewis Research Center (page images at HathiTrust)
• NASA TN D-1846 (National Aeronautics and Space Administration, 1963), by Grady B. Nichols, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Parametric thermodynamic analysis of closed-cycle gas-laser operation in space (National Aeronautics and Space Administration ;, 1974), by Raymond K. Burns and Lewis Research Center (page images at HathiTrust)
• A system for spacecraft attitude control and energy storage (National Aeronautics and Space Administration ;, 1974), by J. D. Shaughnessy and Langley Research Center (page images at HathiTrust)
• Apollo experience report : command and service module electrical power distribution subsystem (National Aeronautics and Space Administration ;, 1974), by Robert E. Munford, Bob Hendrix, and Lyndon B. Johnson Space Center (page images at HathiTrust)
• Endurance testing of downstream cathodes on a low-power MPD thruster (National Aeronautics and Space Administration ;, 1974), by James A. Burkhart, James R. Rose, and Lewis Research Center (page images at HathiTrust)
• Analog computer study of design parameter effects on the stability of a direct-acting gas pressure regulator (National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1971), by Miles O. Dustin (page images at HathiTrust; US access only)
• Preliminary thermal performance analysis of the solar Brayton heat receiver (National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va], 1971), by Raymond K. Burns (page images at HathiTrust)
• Analytical investigation of recirculation-pump and radiator-area requirements for flash vaporization in a turboelectric space power system Arthur J. Glassman. (National Aeronautics and Space Administration :, 1962), by Arthur J. Glassman and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Evaluation of tantalum-alloy-clad uranium mononitride fuel specimens from 7500-hour, 1040 ̊C pumped-lithium-loop test (National Aeronautics and Space Administration ;, 1974), by Gordon K. Watson and Lewis Research Center (page images at HathiTrust)
• Performance of a flight-type laminar radiator with a Brayton power system (National Aeronautics and Space Administration ;, 1974), by Theodore C. Cintula, Robert B. Smith, George M. Prok, and Lewis Research Center (page images at HathiTrust)
• Safe atmosphere entry of an isotope heat source with a single stable trim attitude at hypersonic speeds (National Aeronautics and Space Administration ;, 1972), by Lionel L. Levy, Raymond K. Burns, and Ames Research Center (page images at HathiTrust)
• Apollo experience report : power generation system (National Aeronautics and Space Administration ;, 1973), by David Bell, Fulton M. Plauché, United States National Aeronautics and Space Administration, and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
• Investigation of a 4.0-inch-mean-diameter four-stage reentry turbine for auxiliary power drives (National Aeronautics and Space Administration, 1960), by Robert Y. Wong, Monroe Daniel E., David L. Darmstadt, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Electrical power generation systems for space applications. (Scientific and Technical Information Division, National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1965), by United States National Aeronautics and Space Administration, United States. Aeronautics and Astronautics Coordinating Board. Supporting Research and Technology Panel, and United States. Dept. of Defense (page images at HathiTrust)
• Space Nuclear Power Generators : hearings before the United States Joint Committee on Atomic Energy, Eighty-Ninth Congress, first session, on Aug. 6, 1965. (U.S. G.P.O., 1965), by United States. Congress. Joint Committee on Atomic Energy (page images at HathiTrust)
• Final report-subtask 5.6 : nuclear 1.0-watt power supply for space application. (Office of Scientific and Technical Information, U.S. Dept. of Energy, 1960), by D. J. Knighton, Martin Company. Nuclear Division, and U.S. Atomic Energy Commission. Office of Technical Information (page images at HathiTrust)
• Upper atmosphere re-entry study high altitude burnup : volumn 1 (Martin Marietta, Nuclear Division, 1961), by Phillips N. Brooks, Douglas G. Harvey, Martin Company. Nuclear Division, Martin Marietta Corporation. Nuclear Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Quarterly technical progress report SNAP Aerospace Safety Program (Atomics International ;, 1962), by U.S. Atomic Energy Commission. Technical Information Center and North American Aviation. Atomics International Division (page images at HathiTrust)
• Survey of meteoroid property and distribution data relevant to SNAP 8 reactor and shield design (Canoga Park, California : Atomics International, 1963., 1963), by C. R. Harder, North American Aviation. Atomics International Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Progress report for SNAP (systems for nuclear auxiliary power) general supporting technology... (North American Aviation, Inc. ;, in the 1960s), by U.S. Atomic Energy Commission. Technical Information Center and North American Aviation. Atomics International Division (page images at HathiTrust)
• Energy conversion sytems reference handbook. (Wright Air Development Division, Air Research and Development Command, U.S. Air Force, 1960), by Electro-Optical Systems (Firm) (page images at HathiTrust; US access only)
• Safety analysis report : snaptran 2/10A-1 safety tests (U.S. Atomic Energy Commission, Idaho Operations Office, 1963), by J. M. Waage, Idaho National Reactor Testing Station, Phillips Petroleum Company. Atomic Energy Division, and U.S. Atomic Energy Commission. Idaho Operations Office (page images at HathiTrust)
• Progress report : SNAP systems improvement program, mercury-rankine program, July-September 1966, Volume I. (Downey, California : North American Aviation, Inc., Atomics International Division, 1967., 1967), by North American Aviation. Atomics International Division and U.S. Atomic Energy Commission (page images at HathiTrust)
• Cavity vapor generator program (Wright-Patterson Air Force Base, Ohio : Flight Accessories Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by D. L. Purdy, J. F. Williams, F. A. Blake, R. C. Keyser, United States. Air Force. Systems Command. Aeronautical Systems Division, and General Electric Company. Missile and Space Division (page images at HathiTrust)
• Temperature control technique for solar energy converters (Wright-Patterson Air Force Base, Ohio : Flight Accessories Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by Joel K. Baker, General Electric Company. Missile and Space Division, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Microwave and laser techniques as flight vehicle power transmission subsystems (Wright-Patterson Air Force Base, Ohio : Air Force Aero Propulsion Laboratory, Aeronautical Systems Division, AIr Force Systems Command, United States Air Force, 1963., 1963), by James D. Reams, Air Force Aero Propulsion Laboratory (U.S.), and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Future orbital power systems technology requirements : a symposium held at Lewis Research Center, Cleveland, Ohio, May 31 and June 1, 1978. (National Aeronautics and Space Administration, Scientific and Technical Information Office, 1978), by United States National Aeronautics and Space Administration (page images at HathiTrust)

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