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• An investigation of a device to oscillate a wind-tunnel airstream (National Aeronautics and Space Administration :, 1961), by Charles F. Reid, Clifton Wrestler, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A technique for obtaining hypervelocity impact data by using the relative hypervelocities of two projectiles (National Aeronautics and Space Administration :, 1961), by William H. Kinard, Rufus D. Collins, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA-AEC liquid-metals corrosion meeting December 7-8, 1960, Washington, D.C. (National Aeronautics and Space Administration :, 1961), by United States National Aeronautics and Space Administration (page images at HathiTrust)
• A spectrophotometric attachment for the vacuum ultraviolet / y Norman N. Axelrod. (National Aeronautics and Space Administration :, 1961), by Norman N. Axelrod and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Choosing a suitable sweep rate for sinusoidal vibration testing (National Aeronautics and Space Administration :, 1961), by Neal Granick 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 (National Aeronautics and Space Administration :, 1962), by R. James Rollbuhler, David M. Straight, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Optical torquemeter for high rotational speeds / Alois Kresk Jr. and Marvin Tiefermann. (National Aeronautics and Space Administration :, 1962), by Alois Kresk, Marvin W. Tiefermann, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The theoretical enthalpy distribution of air in steady flow along the axis of a direct-current electric arc (National Aeronautics and Space Administration :, 1962), by Howard A. Stine, Velvin R. Watson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Performance evaluation of fixed- and variable-area rocket exhaust diffusers using single and clustered nozzles with and without gimbaling (National Aeronautics and Space Administration :, 1962), by Bruce E. Church, Richard J. Quentmeyer, William L. Jones, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A 1-foot hypervelocity shock tunnel in which high-enthalpy, real-gas air flows can be generated with flow times of about 180 milliseconds / Bernard E. Cunningham and Samuel Kraus. (National Aeronautics and Space Administration :, 1962), by Bernard E. Cunningham, Samuel Kraus, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The development of an 8-inch by 8-inch slotted tunnel from mach numbers up to 1.28 (National Aeronautics and Space Administration :, 1961), by B. H. Little, James M. Cubbage, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A central facility for recording and processing transient-type data (National Aeronautics and Space Administration :, 1963), by Staff : Lewis Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Receiving system design for the arraying of independently steerable antennas for deep space communications (National Aeronautics and Space Administration :, 1962), by James H. Schrader and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The vector field proton magnetometer for IGY satellite ground stations (National Aeronautics and Space Administration :, 1960), by Ivan R. Shapiro, James P. Heppner, John D. Stolarik, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Determining inertias by using the amplitude decay rate of a mechanical oscillating system (National Aeronautics and Space Administration :, 1962), by Gene T. Carpenter, Dan T. Meredith, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An accelerated reservoir light-gas gun (National Aeronautics and Space Administration :, 1962), by John S. Curtis and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects of surface recombination on heat transfer to bodies in a high enthalpy stream of partially dissociated nitrogen (National Aeronautics and Space Administration :, 1961), by Ernest L. Winkler, Roy N. Griffin, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Design and calibration of an arc-heated, hypersonic, low-density wind tunnel (National Aeronautics and Space Administration :, 1962), by Ruth N. Weitmann 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 (National Aeronautics and Space Administration :, 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. (National Aeronautics and Space Administration :, 1962), by Joseph Weil and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Far-field noise characteristics of Saturn static tests (National Aeronautics and Space Administration :, 1961), by Wade D. Dorland and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Physiological sensors for use in Project Mercury (National Aeronautics and Space Administration :, 1962), by Charles D. Wheelwright and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An analytical and experimental evaluation of a two-stage annular air ejector for high-energy wind tunnels (National Aeronautics and Space Administration :, 1962), by John A. Sheldon, Henry R. Hunczak, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• High-vacuum condenser design: experimental effects from cesium and mercury ion beams (National Aeronautics and Space Administration :, 1962), by Edward A. Richley, Ronald J. Cybulski, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Measurements of flow duration in a low-pressure shock tube (National Aeronautics and Space Administration :, 1962), by Virgil A. Sandborn and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Theory of an electromagnetic mass accelerator for achieving hypervelocities. (National Aeronautics and Space Administration :, 1961), by Karlheinz Thom and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Stability limits of the premixed stoichiometric cyanogen-oxygen flame (National Aeronautics and Space Administration :, 1962), by Irving Fruchtman and United States National Aeronautics and Space Administration (page images at HathiTrust)

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