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PROPULSION SYSTEM PERFORMANCE.

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• Probabilistic modeling for simulation of aerodynamic uncertainties in propulsion systems ([Washington, D.C.] : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1989]), by A. Hamed, United States National Aeronautics and Space Administration, and Lewis Research Center. Institute for Computational Mechanics in Propulsion (page images at HathiTrust)
• Satellite and space propulsion systems / (Washington, D.C. : National Aeronautics and Space Administration, 1960), by Wolfgang E. Moeckel (page images at HathiTrust)
• Radiation measurements and low frequency and high pressure investigations of induction heated plasma / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1971), by Charles E. Vogel, Peter H. Dundas, John W. Poole, Lewis Research Center, and Humphreys Corporation. TAFA Division (page images at HathiTrust)
• Effect of simulated bearing coolant injection on the performance of a two-stage, velocity-compounded turbopump drive turbine / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1967), by Roy G. Stabe, Edward H. Gibbs, John F. Kline, and Lewis Research Center (page images at HathiTrust)
• Experimental investigation of a 4 1/2-stage turbine with very high stage loading factor / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1973-1974), by D. C. Evans, Lewis Research Center, and General Electric Company (page images at HathiTrust)
• Technology requirements for advanced earth orbital transportation systems / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Information Service, 1978-), by A. K. Hepler, E. L. Bangsund, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Control of combustion-chamber pressure and oxidant-fuel ratio for a regeneratively cooled hydrogen-fluorine rocket engine / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by Edward W. Otto, Richard A. Flage, and Lewis Research Center (page images at HathiTrust)
• Analytical comparison of hydrazine with primary propellants as the turbine drive fluid for hydrogen-fluorine and hydrogen-oxygen altitude stage rockets / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by William T. Wintucky and Lewis Research Center (page images at HathiTrust)

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