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Rockets (Aeronautics) -- Nozzles -- Testing

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• Rockets (Aeronautics) -- Nozzles
• Rockets (Aeronautics) -- Testing
• Nozzles -- Testing

• Experimental thrust performance of a high-area-ratio rocket nozzle (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), by Albert J. Pavli, Tamara A. Smith, Kenneth J. Kacynski, and Lewis Research Center (page images at HathiTrust)
• Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m² (350 psia) (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), by Tamara A. Smith, Albert J. Pavli, Lewis Research Center, and Kenneth J. Kacynski (page images at HathiTrust)
• Experimental evaluation of heat transfer on a 1030:1 area ratio rocket nozzle (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), by Kenneth J. Kacynski, Tamara A. Smith, Albert J. Pavli, and Lewis Research Center (page images at HathiTrust)
• Supersonic investigation of nozzle hinge moments of a modified Saturn C-1 model with and without jet flow (National Aeronautics and Space Administration, 1963), by Nickolai Charczenko, Jerry L. Lowery, and Langley Research Center (page images at HathiTrust)
• Performance of a variable divergent-shroud ejector nozzle designed for flight mach numbers up to 3.0 (National Aeronautics and Space Administration, 1961), by Andrew J. Stofan, James R. Mihaloew, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Comparison of rocket performance using exhaust diffuser and conventional techniques for altitude simulation (National Aeronautics and Space Administration, 1959), by Joseph N. Sivo, Daniel J. Peters, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Rocket-nozzle testing and evaluation (Columbus, Ohio : Battelle Memorial Institute, Defense Metals Information Center, 1960., 1960), by E. W. Ungar and Defense Metals Information Center (U.S.) (page images at HathiTrust)

Items below (if any) are from related and broader terms.

• Solid rocket motor nozzles (NASA ;, 1975), by Russell A Ellis (page images at HathiTrust)
• Liquid rocket engine nozzles (National Aeronautics and Space Administration ;, 1976), by Jack C. Hyde, G. S. Gill, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Perfect bell nozzle parametric and optimization curves (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by J. L. Tuttle, D. H. Blount, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Experimental evaluation of several ablative materials as nozzle sections of a storable-propellant rocket engine (National Aeronautical and Space Administration ;, 1966), by Donald A. Peterson, Carl L. Meyer, and Lewis Research Center (page images at HathiTrust)
• Computational study of single-expansion-ramp nozzles with external burning (National Aeronautics and Space Administration ;, 1994), by Shaye Yungster, Charles J. Trefny, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental evaluation of throat inserts in a storable-propellant rocket engine (National Aeronautical and Space Administration ;, 1966), by Jerry M. Winter, James R. Johnston, Larry D. Plews, and Lewis Research Center (page images at HathiTrust)
• Experimental evaluation of a pilot multinozzle-duct apparatus (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by Richard L. Puster, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Langley Research Center (page images at HathiTrust)
• Nonequilibrium gasdynamics (National Aeronautics and Space Administration ;, 1969), by William S. Watt and Cornell Aeronautical Laboratory (page images at HathiTrust)
• A computational model for the prediction of jet entrainment in the vicinity of nozzle boattails (The BOAT code) (National Aeronautics and Space Administration, Scientific and Technical Information Service ;, 1978), by Sanford M. Dash, Harold S. Pergament, Aeronautical Research Associates of Princeton, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• NASA TN D-3561 (National Aeronautics and Space Administration :, 1966), by Gerd Kanning and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-4064 (National Aeronautics and Space Administration ;, 1967), by William F. Hinson, Robert J. McGhee, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6050 (National Aeronautics and Space Administration :, 1970), by Rene E. Chambellan, Eugene J. Pleban, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6060 (National Aeronautics and Space Administration :, 1971), by James M. Cubbage, F. S. Kirkham, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Performance of an isolated two-dimensional wedge nozzle with fixed cowl and variable wedge centerbody at mach numbers up to 2.01 (National Aeronautics and Space Administration ;, 1976), by Donald L. Maiden, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5433 (National Aeronautics and Space Administration ;, 1969), by Dennis M. Bushnell, William V. Feller, William D. Harvey, Charles B. Johnson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental measurements of expanding storable-propellant products simulated by combustion of gaseous reactants (National Aeronautics and Space Administration ;, 1969), by Robert Friedman, Erwin A. Lezberg, Raymond E. Gaugler, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Experimental study of zero-flow ejectors using gaseous nitrogen (National Aeronautics and Space Administration, 1960), by William Leroy Hill Jones, Carl F. Lorenzo, Harold G. Price, and Lewis Research Center (page images at HathiTrust)
• NASA TN D-1742 (National Aeronautics and Space Administration, 1963), by Harvey E. Neumann, Paula J. Bettinger, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Asymmetric "Penshape" nozzles in jet-canard configurations for attitude control (National Aeronautics and Space Administration, 1963), by Robert W. Cubbison and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Preliminary investigation of off-design performance of divergent-ejector-type rocket nozzles (National Aeronautics and Space Administration, 1960), by Laurence W. Gertsma, Richard A. Yeager, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effective thermal conductivities of four metal-ceramic composite coatings in hydrogen-oxygen rocket firings (National Aeronautics and Space Administration ;, 1972), by Ralph L. Schacht, Richard J. Quentmeyer, Harold G. Price, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• NASA TN D-6396 (National Aeronautics and Space Administration :, 1971), by Ralph L. Schacht, Richard J. Quentmeyer, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-6594 (National Aeronautics and Space Administration :, 1972), by Donald R. Boldman, Robert W. Graham, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of a submerged nozzle on a 1/14.2-scale model of the 260-inch solid rocket (National Aeronautics and Space Administration ;, 1967), by Reino J. Salmi, James J. Pelouch, and Lewis Research Center (page images at HathiTrust)
• Experimental evaluation of high-purity-silica reinforced ablative composites as nozzle sections of 7.8-inch-(19.8 CM) diameter throat storable-propellant rocket engine (National Aeronautics and Space Administration ;, 1967), by Donald A. Peterson and Lewis Research Center (page images at HathiTrust)
• Production of tungsten rocket nozzle inserts (U.S. Atomic Energy Commission, Union Carbide Nuclear Company, 1961), by Arthur C. Neeley, Oak Ridge Y-12 Plant, Union Carbide Nuclear Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
• A time-dependent analysis for quasi-one-dimensional nozzle flows with vibrational and chemical nonequilibrium (White Oak, Maryland : United States Naval Ordnance Laboratory, 1969., 1969), by John D. Anderson and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• A time-dependent quasi-one-dimensional analysis of population inversions in an expanding gas (White Oak, Maryland : United States Naval Ordnance Laboratory, 1969., 1969), by John D. Anderson and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• The pressure-carbonization of carbon bonded silicon carbide-graphite for use in uncooled rocket nozzles (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1955., 1955), by Telesphore L. Charland, Bruce R. Goss, James R. Tinklepaugh, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and New York State College of Ceramics at Alfred University (page images at HathiTrust)
• Property determinations for CFW graphite (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), by R. B. Dull, Air Force Materials Laboratory (U.S.), United States. Air Force. Systems Command, and Union Carbide Corporation. Carbon Products Division (page images at HathiTrust)
• A summary of jet plume effects on the stability characteristics of a body of revolution with various fin configurations at Mach numbers from 0.2 to 2.3 : normal jet plume simulator (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research, Development, and Engineering Laboratory, 1976., 1976), by George Batiuk, James H. Henderson, Redstone Arsenal (Ala.), and Development United States. Army. Missile Command. Research (page images at HathiTrust)
• An investigation of the effectiveness of several devices in simulating a rocket plume at free stream Mach numbers 0.9 to 1.2 (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1971., 1971), by James Robert Burt, Redstone Arsenal (Ala.), and United States. Army. Missile Command (page images at HathiTrust)
• Transonic wind tunnel investigation of thrust effects on the longitudinal stability characteristics of several body-fin configurations : sting-mounted model with normal-jet plume simulator (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research, Development, and Engineering Laboratory, 1974., 1974), by James H. Henderson, Redstone Arsenal (Ala.), Chrysler Corporation, and Development United States. Army. Missile Command. Research (page images at HathiTrust)
• An experimental investigation of the interference effects due to a lateral jet issuing from a body of revolution over the Mach number range of 0.8 to 4.5 (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1968., 1968), by Donald J. Spring, Redstone Arsenal (Ala.), and United States. Army. Missile Command (page images at HathiTrust)
• Investigation of jet plume effects on the longitudinal stability characteristics of a body of revolution with various fin configurations at Mach numbers from 0.2 to 2.3 : normal jet plume simulator (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research, Development, and Engineering Laboratory, 1976., 1976), by James H. Henderson, Redstone Arsenal (Ala.), and Development United States. Army. Missile Command. Research (page images at HathiTrust)
• Investigation of the effect of low thrust levels on the base pressure of a cylindrical body at supersonic speeds (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research and Development Directorate, Advanced Systems Labortory, 1970., 1970), by T. A. Martin, C. E. Brazzel, Redstone Arsenal (Ala.), and United States. Army. Missile Command. Research and Development Directorate (page images at HathiTrust)

• Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m² (350 psia) (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), by Tamara A. Smith, Albert J. Pavli, Lewis Research Center, and Kenneth J. Kacynski (page images at HathiTrust)

• NASA TN D-6065 (National Aeronautics and Space Administration :, 1970), by Marvin E. Goldstein, Robert Siegel, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5878 (National Aeronautics and Space Administration :, 1970), by Robert Siegel, Marvin E. Goldstein, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Experimental investigation of the feasibility of ablation-cooling a rocket nozzle with possible application to solid-propellant engines (National Aeronautics and Space Administration, 1961), by Richard R. Cullom and Lewis Research Center (page images at HathiTrust)

• Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m² (350 psia) (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), by Tamara A. Smith, Albert J. Pavli, Lewis Research Center, and Kenneth J. Kacynski (page images at HathiTrust)
• NASA TN D-4471 (National Aeronautics and Space Administration ;, 1968), by W. J. Tuovila, Norman S. Land, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Fabrication of tungsten for solid-propellant rocket nozzles (Columbus, Ohio : Defense Metals Information Center, Battelle Memorial Institute, 1961., 1961), by Robert Isaac Jaffee, V. D. Barth, D. J. Maykuth, and Defense Metals Information Center (U.S.) (page images at HathiTrust)

• Exploring in aerospace rocketry (National Aeronautics and Space Administration, 1968), by William D. Klopp and Lewis Research Center (page images at HathiTrust)
• Rocket-nozzle testing and evaluation (Columbus, Ohio : Battelle Memorial Institute, Defense Metals Information Center, 1960., 1960), by E. W. Ungar and Defense Metals Information Center (U.S.) (page images at HathiTrust)

More items available under broader and related terms at left.