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Propulsion systems, liquid-fuel rockets

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• An analytical approach to the design of an automatic discontinuous control system / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by Lawrence W. Taylor, John W. Smith, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An investigation of the liquid level at the wall of a spinning tank (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by David M. Winch and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Performance of a low-thrust storable propellant rocket at very low chamber pressure / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by John P. Wanhainen, Phil S. Ross, Richard L. DeWitt, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Ignition of a hydrogen-oxygen rocket engine by addition of fluorine to the oxidant / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by R. James Rollbuhler, David M. Straight, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental damping of liquid oscillations in a spherical tank by positive-expulsion bags and diaphragms / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by Andrew J. Stofan, Albert J. Pavli, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Boiling heat transfer to liquid hydrogen and nitrogen in forced flow / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by James P. Lewis, John F. Kline, Jack H. Goodykoontz, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Design and performance of a liquid-hydrogen, liquid-oxygen gas generator for driving a 1000-horsepower turbine / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by Nick J. Sekas, Loren W. Acker, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Base flow characteristics for several four-clustered rocket configurations at mach numbers from 2.0 to 3.5 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Normal T. Musial, James J. Ward, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Stability of titanium nitride and titanium carbide when exposed to hydrogen atoms from 298 degrees to 1950 degrees K / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Warren H. Philipp and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An experimental technique for the investigation of tipoff forces associated with stage separation of multistage rocket vehicles / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Robert L. Gungle, H. Wayne Leonard, William S. Brosier, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An analytical investigation of the loads, temperatures and ranges obtained during the recovery of rocket boosters by means of a parawing / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Howard G. Hatch, William A. McGowan, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Determination of local experimental heat-transfer coefficients on combustion side of an ammonia-oxygen rocket / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Curt H. Liebert and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Annular internal-external-expansion rocket nozzles for large booster applications / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by James F. Connors, Glenn A. Mitchell, Robert W. Cubbison, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Performance of small (100-lb thrust) rockets motors using coaxial injection of hydrazine and nitrogen tetroxide (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Joseph F. Wasserbauer, William Tabata, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Thermodynamic properties of hydrogen from room temperature to 100,000 degrees K / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Burt M. Rosenbaum, Leo Levitt, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Potential-flow analysis of unsteady outflow from a tank and its effect on the dynamics of a fluid system (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by William H. Roudebush, I. Irving Pinkel, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A two-impulse plan for performing rendezvous on a once-a-day basis / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by John D. Bird, David F. Thomas, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Determinations of local and instantaneous combustion conditions from acoustic measurements in a rocket combustor and comparison with overall performance/ (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Martin Hersch and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental study of the effects of weightlessness on the configuration of mercury and alcohol in spherical tanks/ (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Donald A. Petrash, Edward W. Otto, Robert F. Zappa, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Review of the X-15 program Joseph Weil. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Joseph Weil and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Far-field noise characteristics of Saturn static tests / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1961]), by Wade D. Dorland and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analytical and experimental investigation of forces and frequencies resulting from liquid sloshing in a spherical tank Andrew J. Stofan and Alfred L. Armstead. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Andrew J. Stofan, Alfred L. Armstead, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An Empirical correlation of critical boiling heat flux in forced flow upward through uniformly heated tubes Uwe H. von Glahn. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Uwe H. von Glahn and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analytical investigation of performance of two-stage turbine over a range of ratios of specific heats from 1.2 to 1 2/3 Warren J. Whitney and Warner L. Stewart. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Warren J. Whitney, Warner L. Stewart, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analytical performance characteristics and outlet flow conditions of constant and variable lead helical inducers for cryogenic pumps / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by John C. Montgomery and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of the performance of an axial-flow-pump stage designed by the blade-element theory - design and overall performance / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by James E. Crouse, Richard F. Soltis, John C. Montgomery, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Base-flow aerodynamics of a Saturn-type booster stage at mach numbers 0.1 to 2.0 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1962]), by John L. Allen and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Examination of pressure oscillations induced by changes in the burning rate of flames / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by Rose L. Schalla and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Film condensation with and without body force in boundary-layer flow of vapor over a flat plate / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Paul M. Chung and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Optical torquemeter for high rotational speeds / Alois Kresk Jr. and Marvin Tiefermann. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Alois Kresk, Marvin W. Tiefermann, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An experimental determination of the dynamic response of a long hydraulic line / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by John D. Regetz and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of nozzle convergence length on performance of a heptane-oxygen combustor / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Marshall C. Burrows and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A cooled-tube pyrometer with experimental results obtained in a high-temperature gas stream. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by George E. Glawe, Krause,LLyod N., Robert C. Johnson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Propagation of free flames in laminar- and turbulent-flow fields / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Ray E. Bolz, Henry Burlage, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Theory of the fluid oscillations in a circular cylindrical ring tank partially filled with liquid / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Helmut F. Bauer and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental study of effects of geometric variables on performance of conical rocket - engine exhaust nozzles. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Harry E. Bloomer, Pqul E. Renas, Robert J. Antl, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Transfer of cryogenic fluids by an expulsion-bag technique. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Paul J. Sirocky and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental evaluation of analytical models for the inertias and natural frequencies of fuel sloshing in circular cylindrical tanks / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Robert W. Warner, John T. Caldwell, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental performance of nozzles having area ratios up to 300 on JP-4 fuel - liquid-oxygen rocket engine. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by J. Calvin Lovell, Nick E. Samanich, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Combined effect of contraction ratio and chamber pressure on the performance of a gaseous hydrogen liquid oxygen combustor for a given propellant weight flow and oxidant fuel ratio / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Martin Hersch and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Vaporization rates of ethanol sprays in a combustor with low-frequency fluctuations of combustion-gas pressure / Robert D. Ingebo. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Robert D. Ingebo and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Thermodynamic consistency of solubility data for the hydrogen-helium vapor-liquid system / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Irving Brazinsky, Bryon S. Gottfried, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Combustion instability limits determined by a nonlinear theory and a one-dimensional model / by Richard J. Priem and Donald C. Guentert. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], 1962), by Richard J. Priem, Donald C. Guentert, and United States National Aeronautics and Space Administration (page images at HathiTrust)

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