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Filed under: Carnot cycle
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Filed under: Thermodynamic cycles Computer program for thermodynamic performance of Brayton-cycle space-power systems (National Aeronautics and Space Administration ;, 1967), by Arthur J. Glassman and Lewis Research Center (page images at HathiTrust) Computer program for design-point performance of turbojet and turbofan engine cycles (National Aeronautics and Space Administration ;, 1967), by Michael R. Vanco and Lewis Research Center (page images at HathiTrust) NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), by Upshur T. Joyner, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust) On the dimensional instability of uranium and of clad plates subjected to thermal cycling (Washington, D.C. : Office of Technical Services, 1955., 1953), by M. Bettman, J. P. Frankel, G. W. Brown, California Research and Development Company, Lawrence Livermore Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust) Thermodynamic investigation of the benzene turbine cycle (Oak Ridge, Tennessee : U.S. Atomic Energy Commission, Technical Information Service Extension, 1953., 1953), by N. A. Beldecos, J. D. Lokay, U.S. Atomic Energy Commission, and Westinghouse Electric Corporation (page images at HathiTrust)
Filed under: Brayton cycle Computer program for thermodynamic performance of Brayton-cycle space-power systems (National Aeronautics and Space Administration ;, 1967), by Arthur J. Glassman and Lewis Research Center (page images at HathiTrust) Satellite power system : concept development and evaluation program. Volume IV, Energy conversion and power management. (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Lyndon B. Johnson Space Center, and George C. Marshall Space Flight Center (page images at HathiTrust) Design of Brayton rotating unit on rolling- element bearings (National Aeronautics and Space Administration ;, 1969), by R. Cohen, Lewis Research Center, and United Aircraft Corporation. Pratt & Whitney Aircraft Division (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) Design and fabrication of the Brayton rotating unit (National Aeronautics and Space Administration ;, 1972), by J. E. Davis, Lewis Research Center, and AiResearch Manufacturing Company of Arizona (page images at HathiTrust) Alternator and voltage regulator-exciter for a Brayton cycle space power system. I, Design and development (National Aeronautics and Space Administration ;, 1970), by A. M. Dryer, Lewis Research Center, and General Electric Company (page images at HathiTrust) Alternator and voltage regulator-exciter for a Brayton cycle space power system. II, Unbalanced electromagnetic forces (National Aeronautics and Space Administration ;, 1970), by J. E. Greenwell, L. J. Yeager, E. F. Russell, Lewis Research Center, and General Electric Company (page images at HathiTrust) Design, fabrication and testing of a foil gas-bearing test rig (National Aeronautics and Space Administration ;, 1970), by L. Licht, Lewis Research Center, and Ampex Corporation (page images at HathiTrust) Design, fabrication, and performance of foil journal bearing for the brayton rotating unit (National Aeronautics and Space Administration ;, 1973), by Lazar Licht, M. Branger, Lewis Research Center, and Ampex Corporation (page images at HathiTrust) NASA TN D-2487 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1964), by Arthur J. Glassman, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only) NASA TN D-5085 (National Aeronautics and Space Administration ;, 1969), by Lester D. Nichols, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) NASA TN D-5815 (National Aeronautics and Space Administration :, 1970), by Robert Y. Wong, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) NASA TN D-5761 (National Aeronautics and Space Administration :, 1970), by Laurence J. Heidelberg, Carl Weigel, Calvin L. Ball, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only) NASA TN D-5751 (National Aeronautics and Space Administration :, 1970), by Donald C. Guentert, Roy L. Johnsen, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) NASA TN D-4874 (National Aeronautics and Space Administration :, 1968), by Charles S. Corcoran, LeRoy J. Yeager, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) Design of a 3-phase, 15-kilovolt-ampere static inverter for motor-starting a Brayton space power system (National Aeronautics and Space Administration :, 1972), by Robert J. Frye, Arthur G. Birchenough, 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) NASA TN D-6665 (National Aeronautics and Space Administration :, 1972), by David Namkoong, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) One megawatt reactor design for Brayton-cycle space power application. I, Thermal analysis and core design (National Aeronautics and Space Administration ;, 1969), by C. L. Whitmarsh, Paul T. Kerwin, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) NASA TN D-4600 (National Aeronautics and Space Administration ;, 1968), by John L. Klann, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) General reactor sizing techniques aerodynamic optimization (General Electric, Nuclear Materials and Propulsion Operation, 1961), by W.Z. Prickett, U.S. Atomic Energy Commission, and General Electric Company (page images at HathiTrust)
Filed under: Space vehicles -- Auxiliary power supply -- Brayton cycle NASA TN D-2487 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1964), by Arthur J. Glassman, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only) NASA TN D-5815 (National Aeronautics and Space Administration :, 1970), by Robert Y. Wong, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) NASA TN D-6478 (National Aeronautics and Space Administration :, 1971), by Eugene L. Kelsey, Richard N. Young, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) NASA TN D-5924 (National Aeronautics and Space Administration :, 1970), by Bill D. Ingle, Richard C. Bainbridge, Heinz L. Wimmer, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) NASA TN D-5925 (National Aeronautics and Space Administration ;, 1970), by Heinz L. Wimmer, Bill D. Ingle, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) NASA TN D-6513 (National Aeronautics and Space Administration :, 1971), by Lester D. Nichols, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) Performance characteristics of a 14.3-kilovolt-ampere modified Lundell alternator for 1200 hertz Brayton-cycle space-power system (National Aeronautics and Space Administration ;, 1969), by David S. Repas, Richard A. Edkin, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust) Design of a 3-phase, 15-kilovolt-ampere static inverter for motor-starting a Brayton space power system (National Aeronautics and Space Administration :, 1972), by Robert J. Frye, Arthur G. Birchenough, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) NASA TN D-6650 (National Aeronautics and Space Administration :, 1972), by Erwin E. Kempke, Sol H. Gorland, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) NASA TN D-6665 (National Aeronautics and Space Administration :, 1972), by David Namkoong, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) One megawatt reactor design for Brayton-cycle space power application. I, Thermal analysis and core design (National Aeronautics and Space Administration ;, 1969), by C. L. Whitmarsh, Paul T. Kerwin, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) Experimental results of heat transfer and pressure drop of argon flowing through single tube with internal interrupted fins (National Aeronautics and Space Administration, 1967), by David Namkoong, Michael P. Lynch, and Lewis Research Center (page images at HathiTrust) NASA TN D-6525 (National Aeronautics and Space Administration :, 1971), by Paul T. Kerwin, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) Filed under: Otto cycleFiled under: Rankine cycle Mercury droplet size and distribution in glass condenser tube in 1-g and zero- gravity environments (National Aeronautics and Space Administration ;, 1967), by Jonas I. Sturas and Lewis Research Center (page images at HathiTrust) Design and fabrication of noncondensing radiator for environmental evaluation of space power mercury Rankine system (National Aeronautics and Space Administration ;, 1967), by William T. Wintucky, Lockheed Missiles and Space Company, and Lewis Research Center (page images at HathiTrust) Satellite power system : concept development and evaluation program. Volume IV, Energy conversion and power management. (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Lyndon B. Johnson Space Center, and George C. Marshall Space Flight Center (page images at HathiTrust) Three stage potassium vapor turbine test (National Aeronautics and Space Administration ;, 1971), by B. L. Moor, E. Schnetzer, Lewis Research Center, and General Electric Company (page images at HathiTrust) Study of a heat rejection system using capillary pumping (National Aeronautics and Space Administration ;, 1971), by L. G. Neal, O. W. Clausen, D. J. Wanous, Lewis Research Center, and TRW Systems Group (page images at HathiTrust) Three-stage potassium turbine performance test summary (National Aeronautics and Space Administration ;, 1969), by G. C. Wesling, Lewis Research Center, and General Electric Company (page images at HathiTrust) Potassium rankine cycle vapor chamber (heat pipe) radiator study (National Aeronautics and Space Administration ;, 1971), by Ellsworth E. Gerrels, Robert E. Killen, Lewis Research Center, and General Electric Company (page images at HathiTrust) Potassium turboalternator /KTA/ preliminary design study. Volume I, Turbine, bearing, and seal parametric design. (National Aeronautics and Space Administration ;, 1970), by United States National Aeronautics and Space Administration, Lewis Research Center, and AiResearch Manufacturing Company of Arizona (page images at HathiTrust) Potassium turboalternator /KTA/ preliminary design study. Volume II, Alternator parametric design. (National Aeronautics and Space Administration ;, 1970), by United States National Aeronautics and Space Administration and AiResearch Manufacturing Company of Arizona (page images at HathiTrust) NASA TN D-5085 (National Aeronautics and Space Administration ;, 1969), by Lester D. Nichols, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) NASA TN D-4039 (National Aeronautics and Space Administration ;, 1967), by Eugene A. Krejsa, Grady H. Stevens, Jack H. Goodykoontz, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) Analysis of condensing pressure control for SNAP-8 system (National Aeronautics and Space Administration ;, 1966), by Donald R. Packe and Lewis Research Center (page images at HathiTrust) Experimental study of steady-state and dynamic performance of a proportional flueric diverter valve (National Aeronautics and Space Administration ;, 1967), by Milton J. LeRoy and Lewis Research Center (page images at HathiTrust) Rankine and absorption power cycles : selection of fluids for operation between given temperature levels (Oak Ridge, Tennessee : Oak Ridge Gaseous Diffusion Plant, Union Carbide Nuclear Company, 1958., 1958), by A. A. Brooks, A. S. Berman, U.S. Atomic Energy Commission, Union Carbide Nuclear Company, and Oak Ridge Gaseous Diffusion Plant (page images at HathiTrust) Design study (of) electrical component technology for 0.25 to 10.0 megawatt space poser systems : parametric design study of canned ac induction motors (Lima, Ohio : Westinghouse Electric Corporation, Aerospace Electrical Division, 1967., 1967), by T. C Allen, Westinghouse Electric Corporation. Aerospace Electrical Division, and U.S. Atomic Energy Commission (page images at HathiTrust) Implantable power source for circulatory support devices (Waltham, Massachusetts : Thermo Electron Corporation, 1968, 1968), by Thermo Electron Corporation and U.S. Atomic Energy Commission. Division of Isotopes Development (page images at HathiTrust)
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