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Space vehicles -- Thermodynamics

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Filed under: Space vehicles -- Thermodynamics

Radiation heat transfer for spacecraft and solar power plant design. (International Textbook Co., 1962), by Frank Kreith (page images at HathiTrust)
Design of space powerplants. (Prentice-Hall, 1963), by Donald Bawden Mackay (page images at HathiTrust)
Measurement of thermal radiation properties of solids : a symposium held at Dayton, Ohio, September 5, 6, 7, 1962 (Office of Scientific and Technical Information, National Aeronautics and Space Administration : for sale by the Superintendent of Documents, U.S. Govt. Print. Off., 1963), by Dayton Symposium on Measurement of Thermal Radiation Properties of Solids, Joseph C. Richmond, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
Feasibility investigation of a moving belt raditor; summary report. Technical documentary report no. ASD-TDR-63-551. Aeronautical Systems Division, Wright-Patterson Air Force Base, Ohio. BPSN 2-(3-3145)-60853. Prepared under Contract no. AF33(657)-8127. (Clearinghouse for Federal Scientific and Technical Information, U. S. Dept. of Commerce, 1963), by Canoga Park Rocketdyne (page images at HathiTrust)
Analysis of gap heating due to stepped tiles in the shuttle thermal protection system (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by D. H. Petley and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Spectrophotometer-integrating-sphere system for computing solar absorptance (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), by William G. Witte, John E. Perry, Wayne S. Slemp, and Langley Research Center (page images at HathiTrust)
Transient shutdown analysis of low-temperature thermal diodes (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by Richard John Williams, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Ames Research Center (page images at HathiTrust)
Flight test aerodynamic heating data for the afterbody of the Project Mercury spacecraft with comparisons to available prediction methods (National Aeronautics and Space Administration] ;, 1967), by J. D. Murphy, Project Mercury (U.S.), Manned Spacecraft Center (U.S.), Lockheed Missiles and Space Company, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Predisturbed azide base polyurethane foam for rizidization ... (National Aeronautics and Space Administration, 1965), by N. Jouriles, C. E. Welling, Goodyear Aerospace Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Influence of nonequilibrium radiation and shape change on aerothermal environment of a Jovian entry body (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by S. N. Tiwari, S. V. Subramanian, Old Dominion University. Research Foundation, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
On the temperature distribution behind cylinders in a flow (National Aeronautics and Space Administration, 1959), by Ackeret Jakob and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
The design and uncertainty analysis of an improved total hemispherical emittance transient calorimeter (National Aeronautics and Space Administration ;, 1969), by William R. Wade, Donald J. Progar, and Langley Research Center (page images at HathiTrust)
A radiometer for use in thermal studies of spacecraft (National Aeronautics and Space Administration ;, 1968), by George E. Sweet and Howard B. Miller (page images at HathiTrust)
Body motions and angles of attack during Project Fire flight II reentry (National Aeronautics and Space Administration ;, 1967), by William I. Scallion, John H. Lewis, and Langley Research Center (page images at HathiTrust)
Analytical and experimental study of pool heating of liquid hydrogen over a range of accelerations (National Aeronautics and Space Administration :, 1965), by Robert W. Graham, Robert C. Ehlers, Robert C. Hendricks, and Lewis Research Center (page images at HathiTrust)
Apollo experience report : spacecraft heating environment and thermal protection for launch through the atmosphere of the earth (National Aeronautics and Space Administration ;, 1973), by Robert L. Dotts and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
Laminar heat-transfer distributions for a blunted-cone, cone-frustum reentry configuration at Mach 10 (National Aeronautics and Space Administration ;, 1969), by J. David Dearing and Langley Research Center (page images at HathiTrust)
Spectrometric measurements of gas temperatures in arc-heated jets and tunnels (National Aeronautics and Space Administration, 1963), by David H. Greenshields and Langley Research Center (page images at HathiTrust)
Apollo experience report : thermal protection from engine-plume environments (National Aeronautics and Space Administration ;, 1972), by J. Thomas Taylor and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
Structures for reentry heating (National Aeronautics and Space Administration, 1961), by Roger A. Anderson, Robert T. Swann, and Langley Research Center (page images at HathiTrust; US access only)
Experimental study of a hot structure for a reentry vehicle (National Aeronautics and Space Administration, 1961), by Richard A. Pride, Bobbie F. Helms, Dick M. Royster, and Langley Research Center (page images at HathiTrust; US access only)
A comparison of stagnation-point heating in a rocket exhaust to that of actual flight ([Sandia Corp.], 1961), by Frank L. Paris (page images at HathiTrust; US access only)
Test plan optimization for reentry vehicle nose tip evaluation (Albuquerque, New Mexico : Sandia Corporation, Aero-Thermodynamics Department, 1967., 1967), by Roald A. Rindal, Thomas J. Dahm, U.S. Atomic Energy Commission, and Sandia Corporation (page images at HathiTrust)
Development of an analytic model of the response of self-contained, transpiration-cooled nose tips to reentry environments (Albuquerque, New Mexico : Sandia Corporation, Aero-Thermodynamics Department, 1968., 1968), by I. M. Grinberg, E. W. Ungar, W. H. Lane, G. R. Whitacre, U.S. Atomic Energy Commission, and Sandia Corporation (page images at HathiTrust)

Filed under: Space vehicles -- Thermodynamics -- Computer programs

A digital computer program for the dynamic interaction simulation of controls and structure (DISCOS) (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Carl S. Bodley and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)

Filed under: Space vehicles -- Thermodynamics -- Congresses

Current technology for thermal protection systems : proceedings of a workshop (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Stephen J. Scotti, Langley Research Center. Langley Thermophysics Committee, Langley Research Center, United States National Aeronautics and Space Administration, and Current Technology for Thermal Protection Systems Workshop (1992 : Langley Research Center.) (page images at HathiTrust)
11th Space Simulation Conference : proceedings of a symposium held at Lyndon B. Johnson Space Center, Houston, Texas, September 23-25,1980 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by Space Simulation Conference. (11th : 1980 : Lyndon B. Johnson Space Center), United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, United States National Aeronautics and Space Administration, and Institute of Environmental Sciences (page images at HathiTrust)

Filed under: Space vehicles -- Thermodynamics -- Mathematical models

A method of integral relations solution for radiating, nonadiabatic, inviscid flow over a blunt body (National Aeronautics and Space Administration ;, 1969), by John T. Suttles and Langley Research Center (page images at HathiTrust)

Filed under: Space vehicles -- Thermodynamics -- Tables

NASA TN D-4523 (National Aeronautics and Space Administration ;, 1968), by R. W. Patch, Bonnie J. McBride, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)

Filed under: Artificial satellites -- Thermodynamics

Thermal design and thermal data analysis of SA-5 payload (National Aeronautics and Space Administration :, 1965), by Tom C. Bannister, Cliff L. Lumpkin, and George C. Marshall Space Flight Center (page images at HathiTrust)

Filed under: Space stations -- Thermodynamics

Design and testing of a high power spacecraft thermal management system (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), by Michael Edward McCabe, Steve Benner, Jentung Ku, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)

Filed under: Space vehicles -- Atmospheric entry

Dynamics and thermodynamics of planetary entry. (Prentice-Hall, 1963), by W. H. T. Loh (page images at HathiTrust)
Dynamics of atmospheric entry. (McGraw-Hill, 1962), by Robert Clifton Duncan (page images at HathiTrust)
A review of rate constants of selected reactions of interest in re-entry flow fields in the atmosphere (National Bureau of Standards :, 1969), by M. H. Bortner and United States. National Bureau of Standards (page images at HathiTrust)
Hypersonic dynamic stability. (Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, 1967), by General Electric Company (page images at HathiTrust)
Fixed-base and in-flight simulations of longitudinal and lateral-directional handling qualities for piloted re-entry vehicles (Cornell Aeronautical Laboratory, Inc., 1963), by Edwin A. Kidd and Robert P. Harper (page images at HathiTrust)
Pre-development study of a heat flux measurement device suitable for use on flight vehicles (Buffalo, 1962), by Cornell Aeronautical Laboratory and F. A. Vassallo (page images at HathiTrust)
Dispersal of reactor core materials by reentry processes; preliminary analysis (Buffalo, 1962), by Cornell Aeronautical Laboratory and J. L. Beal (page images at HathiTrust)
Mass flow measurement techniques for a flight enthalpy probe. Contract no. P.O.33-531174-G48. (Cornell Aeronautical Laboratory, Inc., 1963), by Donald Ellsworth Adams (page images at HathiTrust)
Chemical kinetics in a reentry flow field, by M. H. Bortner. (Missile and Space Division, General Electric, 1963), by M. H. Bortner and General Electric Company. Missile and Space Division (page images at HathiTrust)
Investigation into more complete use of structural materials through a study of the stress-temperature-time conditions of a re-entry vehicle (Wright Air Development Division, Air Research and Development Command, U. S. Air Force, 1961), by Douglas Aircraft Company and J. E. Davis (page images at HathiTrust)
Optimum shape for transpiration-cooled nosetip of a re-entry vehicle (Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1978), by Kevin E. Yelmgren (page images at HathiTrust)
Investigation of ablation effects on hypersonic dynamic stability of a 10 cone (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967., 1967), by Dave R. Moore, Thomas C. Pope, Charles J. Stalmach, Air Force Flight Dynamics Laboratory (U.S.), and LTV Aerospace Corporation (page images at HathiTrust)
High temperature radome design techniques. (Cornell Aeronautical Laboratory, 1960), by Godfrey F. Buranich (page images at HathiTrust)
Entry probes in the outer solar system; report. (Ames Research Center, National Aeronautics and Space Administration, 1975), by Outer Planet Probe Science Study Group (page images at HathiTrust; US access only)
The High Resolution Accelerometer Package (HiRAP) flight experiment summary for the first 10 flights (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Robert C. Blanchard, K. T. Larman, M. Barrett, and Langley Research Center (page images at HathiTrust)
Aerodynamic pressure and heating-rate distributions in tile gaps around chine regions with pressure at a Mach number of 6.6 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by L. Roane Hunt, Kristopher K. Notestine, and Langley Research Center (page images at HathiTrust)
Effect of interplanetary trajectory options on a manned Mars aerobrake configuration (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Robert D. Braun, Lin C. Hartung, Richard W. Powell, and Langley Research Center (page images at HathiTrust)
Effect of aerodynamic and angle-of-attack uncertainties on the blended entry flight control system of the space shuttle from Mach 10 to 2.5 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by Howard W. Stone, Richard W. Powell, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Exploratory investigation at mach number of 2.01 of the longitudinal stability and control characteristics of a winged reentry configuration (National Aeronautics and Space Administration, 1959), by Gerald V. Foster and United States National Aeronautics and Space Administration (page images at HathiTrust)
Wind-tunnel investigation at high subsonic speed of the static longitudinal stability characteristics of a winged reentry vehicle having a large negatively deflected flap-type control surface (National Aeronautics and Space Administration, 1959), by Paul G. Fournier and United States National Aeronautics and Space Administration (page images at HathiTrust)
Analysis of the space shuttle orbiter entry dynamics from Mach 10 to Mach 2.5 with the November 1976 flight control system (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by Richard W. Powell, Howard W. Stone, and Langley Research Center (page images at HathiTrust)
Structural performance of two aerobrake hexagonal heat shield panel concepts (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by John T. Dorsey, James W. Dyess, and Langley Research Center (page images at HathiTrust)
Effect of aerodynamic and angle-of-attack uncertainties on the May 1979 entry flight control system of the space shuttle from Mach 8 to 1.5 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Howard W. Stone, Richard W. Powell, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
Experimental investigation at Mach 8 of the effects of projections and cavities on heat transfer to a model of the Viking aeroshell (National Aeronautics and Space Administration ;, 1974), by Theodore R. Creel and Langley Research Center (page images at HathiTrust)
Finite-element reentry heat-transfer analysis of space shuttle orbiter (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by William L. Ko, Leslie Gong, Robert D. Quinn, and Ames Research Center (page images at HathiTrust)
Slip-boundary equations for multicomponent nonequilibrium airflow (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Roop N. Gupta, James N. Moss, Carl D. Scott, and Langley Research Center (page images at HathiTrust)
Apparatus for experimental investigation of aerodynamic radiation with absorption by ablation products (National Aeronautics and Space Administration ;, 1977), by William L. Wells, W. L. Snow, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Experimental assessment of a computer program used in space shuttle orbiter entry heating analyses (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by William L. Wells, JoAnn Hudgins, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
Entry dynamics of space shuttle orbiter with longitudinal stability and control uncertainties at supersonic and hypersonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), by Howard W. Stone, Richard W. Powell, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
Entry dynamics of space shuttle orbiter with lateral-directional stability and control uncertainties at supersonic and hypersonic speeds (National Aeronoautics and Space Administration, Scientific and Technical Information Office ;, 1977), by Howard W. Stone, Richard W. Powell, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
Fire I : the reentry heating spacecraft. (National Aeronautics and Space Administration :, 1965), by United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Transonic aerodynamic characteristics of a proposed assured crew return capability (ACRC) lifting-body configuration (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by George M. Ware and Langley Research Center (page images at HathiTrust)
Aerodynamic heating to the gaps and surfaces of simulated reusable-surface-insulation tile arrays in turbulent flow at Mach 6.6 (National Aeronautics and Space Administration ;, 1975), by Irving Weinstein, Andrew J. Chapman, Don E. Avery, and Langley Research Center (page images at HathiTrust)
Static aerodynamic characeristics of a winged single-stage-to-orbit vehicle at Mach numbers from 0.3 to 4.63 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Delma C. Freeman, Roger H. Fournier, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
Stagnation point heat transfer during hypervelocity atmospheric entry (National Aeronautics and Space Administration ;, 1970), by W. S. Rigdon, M. Thomas, R. B. Dirling, McDonnell Douglas Astronautics Company. Western Division, and Langley Research Center (page images at HathiTrust)
An experimental investigation of base heating on typical Mars entry body shapes (National Aeronautics and Space Administration ;, 1971), by O. L. Zappa, William G. Reinecke, Langley Research Center, and Avco Corporation. Systems Division (page images at HathiTrust)
Hollow cathode plasma penetration study (National Aeronautics and Space Administration ;, 1966), by Graham Russell, Elecronics Research Center (U.S.), Bunker-Ramo Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Flight test aerodynamic heating data for the afterbody of the Project Mercury spacecraft with comparisons to available prediction methods (National Aeronautics and Space Administration] ;, 1967), by J. D. Murphy, Project Mercury (U.S.), Manned Spacecraft Center (U.S.), Lockheed Missiles and Space Company, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Aerodynamic effects of bulbous bases (National Aeronautics and Space Administration ;, 1969), by Lars E. Ericsson, J. Peter Reding, Lockheed Missiles and Space Company, and Langley Research Center (page images at HathiTrust)
Magnetohydrodynamics during high speed re-entry. (National Aeronautics and Space Administration, 1965), by P. O. Jarvinen, Avco-Everett Research Laboratory, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Pilot re-entry guidance and control (National Aeronautics and Space Administration, 1965), by Albert B. Miller (page images at HathiTrust; US access only)
High performance hypersonic decelerator for planetary entry (NASA, 1965), by A. C. Kyser, Astro Research Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Coned rotating net (National Aeronautics and Space Administration, 1965), by Richard H. MacNeal, Astro Research Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Rapid methods for calculating radiation transport in the entry environment (National Aeronautics and Space Administration, 1975), by William E. Nicolet, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
Fluctuating surface-pressure characteristics on slender cones in subsonic, supersonic, and hypersonic Mach-number flow (National Aeronautics and Space Administration ;, 1974), by H. Heller, Anthony R. Clemente, Langley Research Center, and Beranek Bolt (page images at HathiTrust)
Analytical comparison of hypersonic flight and wind tunnel viscous/inviscid flow fields (National Aeronautics and Space Administration ;, 1975), by H. J. Fivel, L. J. Mockapetris, R. V. Masek, Langley Research Center, and McDonnell Douglas Astronautics Company-East (page images at HathiTrust)
Experimental plasma studies (National Aeronautics and Space Administration ;, 1972), by M. G. Dunn, Langley Research Center, and Cornell Aeronautical Laboratory (page images at HathiTrust)
Study of critical defects in ablative heat shield systems for the space shuttle (National Aeronautics and Space Administration ;, 1972), by R. L. Thompson, W. E. Driver, Ward D. Rummel, Langley Research Center, and Martin Marietta Denver Aerospace (page images at HathiTrust)
Influence of nonequilibrium radiation and shape change on aerothermal environment of a Jovian entry body (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by S. N. Tiwari, S. V. Subramanian, Old Dominion University. Research Foundation, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
Specification of mesopheric density, pressure, and temperature by extrapolation (National Aeronautics and Space Administration ;, 1973), by M. E. Graves, A. H. Miller, Y. S. Lou, George C. Marshall Space Flight Center, and inc Northrop Services (page images at HathiTrust)
Theoretical and experimental studies of reentry plasmas (National Aeronautics and Space Administration ;, 1973), by M. G. Dunn, Sang-Wook Kang, Langley Research Center, and Cornell Aeronautical Laboratory (page images at HathiTrust)
Aerobrake concepts for NTP systems study (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Manuel I. Cruz, Langley Research Center, and TRW Inc. Space and Technology Group (page images at HathiTrust)
Effects of precursor heating on radiative and chemially reacting viscous flow around a Jovian entry body (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by S. N. Tiwari, Kuo-Yen Szema, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
NASA TR R-151 (National Aeronautics and Space Administration ;, 1963), by Rodney C. Wingrove, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
NASA TR R-62 (National Aeronautics and Space Administration ;, 1960), by Leonard Roberts, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Coupled vibration and dissociation relaxation behind strong shock waves in carbon dioxide (National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1967), by Franz Hindelang (page images at HathiTrust; US access only)
Trajectory optimization for an Apollo-type vehicle under entry conditions encountered during lunar return (National Aeronautics and Space Administration, 1967), by John W. Young and Robert L. Smith (page images at HathiTrust; US access only)
NASA TR R-259 (National Aeronautics and Space Administration ;, 1967), by Paul F. Holloway, E. Brian Pritchard, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
NASA TR R-260 (National Aeronautics and Space Administration ;, 1967), by Paul F. Holloway, E. Brian Pritchard, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
The Effect of lift on entry corridor depth and guidance requirements for the return lunar flight (U.S. G.P.O., 1961), by Thomas J. Wong, Robert E. Slye, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
Trajectory control for vehicles entering the earth's atmosphere at small flight-path angles (U.S. G.P.O., 1961), by John M. Eggleston, John W. Young, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
Calculated radio attenuation due to plasma sheath on hypersonic blunt-nosed cone (National Aeronautics and Space Administration, 1963), by John S. Evans, Paul W. Huber, and Langley Research Center (page images at HathiTrust)
NASA TN D-2049 (National Aeronautics and Space Administration, 1963), by Jack A. White, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
NASA TN D-2033 (National Aeronautics and Space Administration, 1963), by Bernard Spencer, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
NASA TN D-1980 (National Aeronautics and Space Administration, 1963), by George E. Kaattari, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
A theory of space-probe entry under conditions of high mass loss (National Aeronautics and Space Administration ;, 1963), by Frederick C. Grant and United States National Aeronautics and Space Administration (page images at HathiTrust)
Determination of effects of oxidation on performance of charring ablators (National Aeronautics and Space Administration [For sale by the Office of Technical Services, Dept. of Commerce, Washington, D.C. 20230], 1964), by Marvin B. Dow, Robert T. Swann, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
NASA TN D-2076 (National Aeronautics and Space Administration, 1963), by Donald E. Holeski, William T. Wintucky, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
NASA TN D-2064 (National Aeronautics and Space Administration, 1963), by Fred A. Demele, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Pressure gradient effects on heat transfer to reusable surface insulation tile-array gaps (National Aeronautics and Space Administration ;, 1975), by David A. Throckmorton and Langley Research Center (page images at HathiTrust)
Aerothermal performance and structural integrity of a René 41 thermal protection system at Mach 6.6 (National Aeronautics and Space Administration ;, 1975), by William D. Deveikis and Langley Research Center (page images at HathiTrust)
Apollo experience report : guidance and control systems : command and service module entry monitor subsystem (National Aeronautics and Space Administration ;, 1975), by Ben Reina, Herbert G. Patterson, and Lyndon B. Johnson Space Center (page images at HathiTrust)
An Analysis of errors and requirements of an optical guidance technique for approaches to atmospheric entry with interplanetary vehicles (U.S. G.P.O., 1961), by David P. Harry and Alan L. Friedlander (page images at HathiTrust)
Z functions (U.S. Govt. Print. Off., 1961), by Dean Roden Chapman and Arline K. Kapphahn (page images at HathiTrust)
NASA TN D-2420 (National Aeronautics and Space Administration :, 1964), by Edwin J. Saltzman, United States National Aeronautics and Space Administration, and Flight Research Center (U.S.) (page images at HathiTrust; US access only)
Survey of energy-absorption devices for soft landing of space vehicles (National Aeronautics and Space Administration :, 1962), by Jack B. Esgar and United States National Aeronautics and Space Administration (page images at HathiTrust)
Effects of simulated retrorockets on the aerodynamic characteristics of a body of revolution at Mach numbers from 0.25 to 1.90 (National Aeronautics and Space Administration :, 1962), by Victor L. Peterson, Robert L. McKenzie, and United States National Aeronautics and Space Administration (page images at HathiTrust)
NASA TN D-4028 (National Aeronautics and Space Administration ;, 1967), by Fred R. DeJarnette, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
The atmospheric transmission of infrared radiation from 2-5 microns for slant paths from 35,000 feet to the upper limit of the atmosphere, a survey (National Aeronautics and Space Administration ;, 1967), by Herbert L. Richard (page images at HathiTrust)
NASA TN D-4065 (National Aeronautics and Space Administration ;, 1967), by Ronald C. Smith, Alan D. Levin, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
NASA TN D-4443 (National Aeronautics and Space Administration ;, 1968), by Dennis M. Bushnell, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
A parametric study of the aerodynamic characteristics of nose-cylinder-flare bodies at a Mach number of 6.0 (National Aeronautics and Space Administration ;, 1965), by George C. Ashby, Aubrey M. Cary, and Langley Research Center (page images at HathiTrust)
Analysis of melting boundary layers on decelerating bodies (National Aeronautics and Space Administration :, 1962), by Simon Ostrach, Jesse Hamman, Arthur W. Goldstein, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Radio transmission through the plasma sheath around a lifting reentry vehicle (National Aeronautics and Space Administration :, 1961), by Macon C. Ellis, Paul W. Huber, and Langley Research Center (page images at HathiTrust)
A flight measurement of optical radiation from shock-heated air by using a Trailblazer II vehicle (National Aeronautics and Space Administration ;, 1968), by Lloyd S. Keafer, Ernest E. Burcher, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
Viking entry vehicle aerodynamics at M = 2 in air and some preliminary test data for flight in CO₂ at M = 11 (National Aeronautics and Space Administration ;, 1975), by Robert I. Sammonds, Robert L. Kruse, and Ames Research Center (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-5769 (National Aeronautics and Space Administration ;, 1970), by Stephen S. Tompkins, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
NASA TN D-5766 (National Aeronautics and Space Administration :, 1970), by Michael C. Fischer, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
NASA TN D-5792 (National Aeronautics and Space Administration ;, 1970), by Walter B. Olstad, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Effect of simulated earth reentry exposure on mechanical properties of several oxide dispersion strengthened and superalloy sheet materials (National Aeronautics and Space Administration ;, 1977), by J. Daniel Whittenberger and United States National Aeronautics and Space Administration (page images at HathiTrust)
NASA TN D-5365 (National Aeronautics and Space Administration ;, 1969), by James F. Campbell, Josephine W. Grow, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
NASA TN D-5701 (National Aeronautics and Space Administration ;, 1970), by George E. Weeks, Joseph E. Waltz, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Radio blackout alleviation and plasma diagnostic results from a 25,000 foot per second blunt-body reentry (National Aeronautics and Space Administration ;, 1970), by Norman D. Akey, Aubrey E. Cross, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
The aerothermodynamic environment of the Apollo command module during suborbital entry (National Aeronautics and Space Administration ;, 1972), by Dorothy B. Lee, Winston D. Goodrich, and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
Calculation of laminar heat transfer to the windward surfaces of straight wing shuttle vehicles at high angle of attack and with yaw (National Aeronautics and Space Administration ;, 1972), by C. C. Pappas, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
Wind-tunnel investigation of the aerodynamic pressures on the Apollo command module configuration (National Aeronautics and Space Administration ;, 1969), by William C. Moseley, B. J. Wells, United States National Aeronautics and Space Administration, and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
Polynomial approximations of thermodynamic properties of arbitrary gas mixtures over wide pressure and density ranges (National Aeronautics and Space Administration ;, 1972), by Dennis O. Allison and Langley Research Center (page images at HathiTrust)
Entry aerodynamics at lunar return conditions obtained from the flight of Apollo 4 (AS-501) (National Aeronautics and Space Administration ;, 1969), by E. R. Hillje, United States National Aeronautics and Space Administration, and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
NASA TN D-4976 (National Aeronautics and Space Administration ;, 1969), by Philip R. Nachtsheim, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
A study of the aerodynamic characteristics of a fixed geometry paraglider configuration and three canopies with simulated variable canopy inflation at a mach number of 6.6 (National Aeronautics and Space Administration :, 1962), by Jim A. Penland and United States National Aeronautics and Space Administration (page images at HathiTrust)
Geomagnetic- and interplanetary-magnetic-field environment of an earth satellite (National Aeronautics and Space Administration :, 1962), by Edward W. Leyhe and United States National Aeronautics and Space Administration (page images at HathiTrust)
Motion and heating during atmosphere reentry of space vehicles (National Aeronautics and Space Administration, 1960), by Thomas J. Wong, Robert E. Slye, Glen Goodwin, and Ames Research Center (page images at HathiTrust; US access only)
Longitudinal aerodynamic characteristics of two blunted cone reentry configurations at Mach numbers from 17.6 to 22.2 including some Reynolds number effects (National Aeronautics and Space Administration ;, 1966), by Dal V. Maddalon and Langley Research Center (page images at HathiTrust)
Aerodynamic damping and oscillatory stability in pitch and yaw of Gemini configurations at Mach numbers from 0.50 to 4.63 (National Aeronautics and Space Administration ;, 1966), by Bruce R. Wright, Robert A. Kilgore, and Langley Research Center (page images at HathiTrust)
Heat-transfer and pressure distributions for laminar separated flows downstream of rearward-facing steps with and without mass suction (National Aeronautics and Space Administration ;, 1974), by Ronald D. Brown, Antoni K. Jakubowski, and Langley Research Center (page images at HathiTrust)
Flight test of an erectable spacecraft used for decelerator testing at simulated Mars entry conditions (National Aeronautics and Space Administration ;, 1972), by Allen B. Henning, Reginald R. Lundstrom, and Langley Research Center (page images at HathiTrust)
Hypersonic aerodynamics and entry-maneuver--aerothermodynamic interactions for two lifting entry vehicles (National Aeronautics and Space Administration ;, 1972), by James P. Arrington, William C. Woods, and Langley Research Center (page images at HathiTrust)
Some landing studies pertinent to glider-reentry vehicles (National Aeronautics and Space Administration :, 1960), by John C. Houbolt, Sidney A. Batterson, and Langley Research Center (page images at HathiTrust)
Atomization, drop size, and penetration for cross-stream water injection at high-altitude reentry conditions with application to the RAM C-I and C-III flights (National Aeronautics and Space Administration ;, 1972), by Paul B. Gooderum, Dennis M. Bushnell, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
Flight tests of Viking parachute system in three Mach number regimes (National Aeronautics and Space Administration ;, 1974), by Reginald R. Lundstrom and Langley Research Center (page images at HathiTrust)
Subsonic and transonic pressure distributions around a bluff afterbody in the wake of a 120⁰ cone for various separation distances (National Aeronautics and Space Administration :, 1971), by James Wayne Sawyer, Charles F. Whitcomb, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Sonic-boom ground-pressure measurements from Apollo 15 (National Aeronautics and Space Administration ;, 1972), by David A. Hilton, Royce L. McKinney, Herbert R. Henderson, and Langley Research Center (page images at HathiTrust)
A real-gas study of low-density wedge-induced laminar separation on a highly cooled blunt flat plate at M [infinity]=12 (National Aeronautics and Space Administration, 1968), by John Benjamin Anders and C. L. W. Edwards (page images at HathiTrust)
Experimental stability and control results at Mach 19 of an entry vehicle designed for an intermediate lift-drag ratio (National Aeronautics and Space Administration ;, 1968), by Patrick J. Johnston, Robert D. Witcofski, and Langley Research Center (page images at HathiTrust)
Body motions and angles of attack during Project Fire flight II reentry (National Aeronautics and Space Administration ;, 1967), by William I. Scallion, John H. Lewis, and Langley Research Center (page images at HathiTrust)
Entry flight aerodynamics from Apollo Mission AS-202 (National Aeronautics and Space Administration ;, 1967), by E. R. Hillje and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
Static longitudinal aerodynamic characteristics at transonic speeds and angles of attack up to 99 degree of a reentry glider having folding wing-tip panels (National Aeronautics and Space Administration, 1961), by Walter B. Olstad and Langley Research Center (page images at HathiTrust)
Preliminary investigation of modified blunt 13 degree half-cone re-entry configurations at subsonic speeds (National Aeronautics and Space Administration, 1961), by George C. Kenyon, George G. Edwards, and Ames Research Center (page images at HathiTrust)
Investigation of the static stability characteristics of a reentry spacecraft model in free flight for Mach numbers from 2.62 to 1.11 launched at an angle of attack of 180 degree (National Aeronautics and Space Administration, 1961), by J. W. Usry and Langley Research Center (page images at HathiTrust)
Effectiveness of several control arrangements on a Mercury-type capsule (National Aeronautics and Space Administration, 1961), by Robert I. Sammonds, Robert R. Dickey, and Ames Research Center (page images at HathiTrust)
Approximate analysis of G loads and heating during atmospheric entries and passes with constant aerodynamic coefficients Roger W. Luidens. (National Aeronautics and Space Administration :, 1962), by Roger W. Luidens and United States National Aeronautics and Space Administration (page images at HathiTrust)
Static structural tests of a 1.5-meter-diameter fabric attached inflatable decelerator (National Aeronautics and Space Administration ;, 1972), by Conrad M. Willis, Martin M. Mikulas, and Langley Research Center (page images at HathiTrust)
Investigation of the response of multiweb beams to static and dynamic loading. Wilbur B. Fichter and Eldon E. Kordes. (National Aeronautics and Space Administration :, 1962), by W. B. Fichter, Eldon E. Kordes, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Experimental investigation of a plasma-covered cavity-backed slot antenna (National Aeronautics and Space Administration ;, 1969), by Thomas G. Campbell, William F. Croswell, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
A theoretical and experimental study of hypersonic flow over flared bodies at incidence (National Aeronautics and Space Administration ;, 1966), by John V. Rakich, Gene P. Menees, and Ames Research Center (page images at HathiTrust)
Spectrographic temperature measurements in a carbon-arc-powered air jet (National Aeronautics and Space Administration, 1959), by David H. Greenshields and Langley Research Center (page images at HathiTrust)
Evaluation of flow properties behind 120-̊ and 140-̊included-angle cones and a Viking '75 entry vehicle at Mach numbers from 1.60 to 3.95 (National Aeronautics and Space Administration ;, 1973), by Clarence A. Brown, James F. Campbell, and Langley Research Center (page images at HathiTrust)
Sonic-boom ground pressure measurements from the launch and reentry of Apollo 16 (National Aeronautics and Space Administration ;, 1974), by Herbert R. Henderson, David A. Hilton, and Langley Research Center (page images at HathiTrust)
NASA TN D-6269 (National Aeronautics and Space Administration:, 1971), by Kenneth W. McAlister (page images at HathiTrust; US access only)
Centered 1-D unsteady expansion of a vibrationally relaxing nitrogen-oxygen mixture (National Aeronautics and Space Administration :, 1967), by Laurence N. Connor, Frances W. Taylor, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
NASA TN D-3871 (National Aeronautics and Space Administration :, 1967), by James C. Dunavant, Howard W. Stone, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Effects of 2 vibration-dissociation coupling models on nonequilibrium hypersonic flow of nitrogen over a wedge (National Aeronautics and Space Administration :, 1966), by Fred R. DeJarnette and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
NASA TN D-3631 (National Aeronautics and Space Administration :, 1966), by Paul E. Tippens, John R. Davidson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
NASA TN D-2880 (National Aeronautics and Space Administration :, 1965), by F. O. Vonbun and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
NASA TN D-4122 (National Aeronautics and Space Administration ;, 1967), by Jim A. Penland, Peter T. Bernot, and United States National Aeronautics and Space Administration (page images at HathiTrust)
NASA TN D-4118 (National Aeronautics and Space Administration ;, 1967), by Paul W. Huber and United States National Aeronautics and Space Administration (page images at HathiTrust)
NASA TN D-5193 (National Aeronautics and Space Administration ;, 1969), by Barbara J. Short, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
NASA TN D-1617 (National Aeronautics and Space Administration, 1963), by Gene W. Sparrow, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
NASA TN D-4494 (National Aeronautics and Space Administration ;, 1968), by W. Douglas Morris, Lana M. Couch, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Guidance and control during direct-descent parabolic reentry (National Aeronautics and Space Administration, 1961), by Edwin C. Foudriat, Rodney C. Wingrove, United States National Aeronautics and Space Administration, Ames Research Center, Langley Research Center, and D.C.) NASA-Industry Apollo Technical Conference (1961 : Washington (page images at HathiTrust)
NASA TN D-1961 (National Aeronautics and Space Administration, 1963), by Albin O. Pearson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Approximate analysis of atmospheric entry corridors and angles (National Aeronautics and Space Administration, 1961), by Roger W. Luidens and Lewis Research Center (page images at HathiTrust)
An analysis of the lunar return mission (National Aeronautics and Space Administration :, 1963), by John P. Gapcynski, Robert H. Tolson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Curve fits of predicted inviscid stagnation-point radiative heating rates, cooling factors, and shock standoff distances for hyperbolic earth entry (National Aeronautics and Space Administration ;, 1974), by John T. Suttles, Stephen B. Margolis, Edward M. Sullivan, and Langley Research Center (page images at HathiTrust)
An analysis of atmospheric entry trajectories for manned and unmanned missions to the planet Venus (National Aeronautics and Space Administration ;, 1973), by Mark K. Craig, Ralph G. Gonzalez, United States National Aeronautics and Space Administration, and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
Boundary-layer electron profiles for entry of a blunt slender body at high altitude (National Aeronautics and Space Administration ;, 1973), by John S. Evans, Paul W. Huber, Charles J. Schnexnayder, and Langley Research Center (page images at HathiTrust)
Safe atmosphere entry of an isotope heat source with a single stable trim attitude at hypersonic speeds (National Aeronautics and Space Administration ;, 1972), by Lionel L. Levy, Raymond K. Burns, and Ames Research Center (page images at HathiTrust)
Apollo experience report : aerothermodynamics evaluation (National Aeronautics and Space Administration ;, 1972), by Dorothy B. Lee and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
Chemical nonequilibrium effects on the inviscid flow in the windward plane of symmetry of two simplified shuttle configurations (National Aeronautics and Space Administration ;, 1973), by John A. Lordi, Charles B. Johnson, Robert J. Vidal, and Langley Research Center (page images at HathiTrust)
A method for predicting shock shapes and pressure distributions on two-dimensional airfoils at large angles of attack (National Aeronautics and Space Administration ;, 1973), by George E. Kaattari and Ames Research Center (page images at HathiTrust)
Manual-control simulation study of a nonlifting vehicle during orbit, retro-rocket firing, and reentry into the earth's atmosphere (National Aeronautics and Space Administration, 1960), by Roger M. Davidson, Jack T. Kaylor, Donald C. Cheatham, and Langley Research Center (page images at HathiTrust)
Effect of wing sweep, angle of attack, Reynolds number, and wing root fillet on the interference heating to the wing windward surface of an entry vehicle configuration (National Aeronautics and Space Administration ;, 1972), by Louis E. Clark, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
Use of hexafluoroethane to simulate the inviscid real-gas effects on blunt entry vehicles (National Aeronautics and Space Administration ;, 1974), by James L. Hunt, Kathryn A. Smith, Robert A. Jones, and Langley Research Center (page images at HathiTrust)
Ablative performance of uncoated silicone-modified and shuttle baseline reinforced carbon composites (National Aeronautics and Space Administration ;, 1976), by Dennis L. Dicus, Ronald D. Brown, Russell N. Hopko, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
The effect of finite thrust and heating constraints on the synergetic plane change maneuver for a space shuttle orbiter-class vehicle (National Aeronautics and Space Administration ;, 1973), by Ernst Dieter Dickmanns and George C. Marshall Space Flight Center (page images at HathiTrust)
Pressure and heat-transfer distribution on the afterbody of a lifting Mercury-type capsule at Mach number 15 in helium (National Aeronautics and Space Administration, 1963), by Joseph G. Marvin and Ames Research Center (page images at HathiTrust)
Static longitudinal and lateral stability and control characteristics of a right triangular pyramidal lifting reentry configuration at Mach numbers from 2.36 to 4.65 (National Aeronautics and Space Administration, 1963), by Nickolai Charczenko, C. Donald Babb, and Langley Research Center (page images at HathiTrust)
Static aerodynamic characteristics of a 1/9-scale model of the escape and exit configurations of the Project Mercury spacecraft at Mach numbers from 2.30 to 4.65 (National Aeronautics and Space Administration, 1962), by Roger H. Fournier and Langley Research Center (page images at HathiTrust)
Static longitudinal aerodynamic characteristics at a Mach number of 10.03 of low-aspect-ratio wing-body configurations suitable for reentry (National Aeronautics and Space Administration, 1962), by Lawrence E. Putnam, Cuyler W. Brooks, and Langley Research Center (page images at HathiTrust)
Wind-tunnel investigation at a Mach number of 2.91 of stability and control characteristics of three lifting reentry configurations at angles of attack up to 90 degrees (National Aeronautics and Space Administration, 1961), by John E. Grimaud and Langley Research Center (page images at HathiTrust)
Static longitudinal aerodynamic characteristics at transonic speeds of a lenticular-shaped reentry vehicle (National Aeronautics and Space Administration, 1960), by John P. Mugler, Walter B. Olstad, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Wind-tunnel investigation of static aerodynamic characteristics of a 1/9-scale model of a possible reentry capsule at mach numbers from 2.29 to 4.65 (National Aeronautics and Space Administration, 1959), by David S. Shaw, Kenneth L. Turner, and United States National Aeronautics and Space Administration (page images at HathiTrust)
An analysis of the stability of spinning disks during atmosphere reentry (National Aeronautics and Space Administration, 1960), by J. Douglas Birdwell, Charles P. LLewellyn, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Experimental investigation of a disk-shaped reentry configuration at transonic and low supersonic speeds (National Aeronautics and Space Administration, 1962), by Frank A. Lazzeroni and United States National Aeronautics and Space Administration (page images at HathiTrust)
Investigation of the low-subsonic stability and control characteristics of a 0.34-scale free-flying model of a modified half-cone reentry vehicle (National Aeronautics and Space Administration, 1962), by James L. Hassell, George M. Ware, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Static longitudinal and lateral stability characteristics at a mach number of 3.11 of square and circular plan-form reentry vehicles, with some effects of controls and leading-edge extensions (National Aeronautics and Space Administration, 1960), by Byron M. Jaquet and United States National Aeronautics and Space Administration (page images at HathiTrust)
Dynamic stability and dispersion of a Project Mercury test capsule upon entering the atmosphere, with effects of roll rate, center-of-gravity displacement, and threshold of a rate-reaction control system (National Aeronautics and Space Administration, 1961), by Byron M. Jaquet, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Effect of longitudinal and lateral controls on winged reentry configuration at mach 1.97 and angles of attack up to 90° (National Aeronautics and Space Administration, 1961), by Gerald V. Foster and United States National Aeronautics and Space Administration (page images at HathiTrust)
Subsonic aerodynamic characteristics of disk re-entry configurations with elliptic cross sections and thickness-diameter ratios of 0.225 and 0.325 (National Aeronautics and Space Administration, 1961), by Fred A. Demele, Jack J. Brownson, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Effects of transverse center-of-gravity displacement, afterbody geometry, and front-face curvature on the aerodynamic characteristics of Mercury-type models at a mach number of 5.5 (National Aeronautics and Space Administration, 1961), by Peter F. Intrieri and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Free-flight measurements of static and dynamic stability of models of the Project Mercury re-entry capsule at Mach numbers 3 and 9.5 (National Aeronautics and Space Administration, 1960), by Simon C. Sommer, Dale L. Compton, Barbara J. Short, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Upper atmosphere re-entry study high altitude burnup : volumn 1 (Martin Marietta, Nuclear Division, 1961), by Phillips N. Brooks, Douglas G. Harvey, Martin Company. Nuclear Division, Martin Marietta Corporation. Nuclear Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
Aerospace safety reentry analytical and experimental program SNAP 2 and 10A : (interim report) (Canoga Park, California : Atomics International, 1963., 1963), by R. D. Elliott, North American Aviation. Atomics International Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
Interlevel correlations of temperature and density, surface to 60 km. (Air Force Geophysics Laboratory, 1980), by Allen E. Cole, Eugene A. Bertoni, and Arthur J. Kantor (page images at HathiTrust)
Proceedings. [David M. Jones, Symposium chairman] (Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962), by Ohio) Symposium on Aerothermoelasticity (1st : 1961 : Dayton, David M. Jones, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust; US access only)
Gas dynamics in space exploration ; [scientific papers] (National Aeronautics and Space Administration, Office of Scientific and Technical Information ; [for sale by the Superintendent of Documents, U.S.Govt. Print.Off.], 1963), by Chicago NASA-University Conference on the Science and Technology of Space Exploration (page images at HathiTrust)
Radiative heating of vehicles entering the earth's atmosphere (National Aeronautics and Space Administration, 1962), by Bradford H. Wick and North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development (page images at HathiTrust)
Wave propagation in a warm magnetoplasma with Coulomb interactions (L.G. Hanscom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, United States Air Force, 1970., 1970), by Robert J. Papa and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
Extension of Dougherty's Model Fokker-Planck Equation for a Plasma (L.G. Hanscom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, United States Air Force, 1970., 1970), by Robert J. Papa and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
A simple method of simulating motion and plasma induced variations in the attenuation of signals transmitted from reentry vehicles (L.G. Hanscom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1973., 1973), by J. L. Poirier, D. H. Tropea, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
Techniques for measuring liquid water content along a trajectory (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), by Rosemary M. Dyer, Y. Izumi, R. O. Berthel, and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
Time and space variation of density in the tropics (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1979., 1979), by Arthur J. Kantor, Allen E. Cole, and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
Interlevel correlations of temperature and density, surface to 60 km (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1980., 1980), by Allen E. Cole, Eugene A. Bertoni, Arthur J. Kantor, and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
Wind distributions and interlevel correlations, surface to 60 km (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1980., 1980), by Arthur J. Kantor, Allen E. Cole, and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
On hypersonic blunt body flow fields obtained with a time-dependent technique (White Oak, Maryland : United States Naval Ordnance Laboratory, 1968., 1968), by John D. Anderson, Allen E. Winkelmann, Lorenzo M. Albacete, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
Oblique shock interaction experiments (White Oak, Maryland : United States Naval Ordnance Laboratory, 1969., 1969), by David L. Merritt, Philip M. Aronson, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
Investigation of substructure heating on cracked ablative heat shields (White Oak, Maryland : United States Naval Ordnance Laboratory, 1969., 1969), by Erhard M. Winkler, M. T. Madden, J. A. Koenig, Richard L. Humphrey, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
Supersonic ablation studies with teflon (White Oak, Maryland : United States Naval Ordnance Laboratory, 1969., 1969), by Erhard M. Winkler, J. A. Koenig, Richard L. Humphrey, M. T. Madden, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
Measurements of blast-induced transient pressures at the base of a cone in supersonic flow (White Oak, Maryland : United States Naval Ordnance Laboratory, 1969., 1969), by Frank P. Baltakis, Gary D. Senechal, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
A computer program for the interception of a re-entry body by a ground-launched interceptor (White Oak, Maryland : United States Naval Ordnance Laboratory, 1969., 1969), by E. L. Harris, Carolyn H. Piper, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
Shock interaction surface pressures for hemispherical and conical bodies (White Oak, Maryland : United States Naval Ordnance Laboratory, 1971., 1971), by Frank P. Baltakis and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
The prediction of aerodynamic heating of fins on re-entry vehicles (Albuquerque, New Mexico : Sandia Laboratories, Aerothermodynamics Division, 1971., 1971), by E. C. Lemmon, U.S. Atomic Energy Commission, and Sandia Laboratories (page images at HathiTrust)
Summary of static stability and drag characteristics of axisymmetric low-drag shapes for the subsonic to hypersonic mach number range (Albuquerque, New Mexico : Sandia Laboratories, Experimental Aerodynamics Laboratories, 1968., 1968), by Amado A. Trujillo, U.S. Atomic Energy Commission, and Sandia Corporation (page images at HathiTrust)
Decomposition kinetics of the phenolic-carbon cloth FM 5055A ablator : II, Rate controlling reactions : consecutive second order (Albuquerque, New Mexico : Sandia Laboratories, 1968, 1968), by I. Auerbach, U.S. Atomic Energy Commission, and Sandia Corporation (page images at HathiTrust)
Base impellers for roll control of reentry vehicles (Albuquerque, New Mexico : Sandia Laboratories, 1969., 1969), by M. D. Bennett, Amado A. Trujillo, U.S. Atomic Energy Commission, and Sandia Corporation (page images at HathiTrust)
In-flight simulation of the lateral-directional handling qualities of entry vehicles (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, U.S. Air Force, 1961., 1961), by Robert P. Harper, United States. Air Force. Air Research and Development Command, Wright Air Development Division, Cornell Aeronautical Laboratory, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
Derivation of sufficient conditions for application of the distorted-wave born approximation to turbulent wake backscatter (Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1974), by Ronald L. Fante and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
Interpretation of microwave antenna results from a reentry flight test : a comparison of methods (Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1974), by John F. Lennon, J. Leon Poirier, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
Investigation of numerical techniques for predicting aerodynamic heating to flight vehicles (Wright-Patterson Air Force Base : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1979., 1979), by Arthur B. Lewis, Neil J. Sliski, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
Fixed-base in-flight simulations of longitudinal and lateral-directional handling qualities for piloted re-entry vehicles (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), by Edwin A. Kidd, Robert P. Harper, Wright-Patterson Air Force Base (Ohio), Cornell Aeronautical Laboratory, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
Effects of different flow field conditions on the high power transmission properties of a reentry plasma (Air Force Cambridge Research Laboratories, Air Force System Command, United States Air Force, 1973), by Robert J. Papa, Richard L. Taylor, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
Proceedings of Symposium on Aerothermoelasticity ; 30-31 October and 1 November 1961 (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, [1962], 1962), by David M. Jones and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
Beryllium composite structures. Volume 2, Materials and processes (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by James N. Krusos, Aeronca Aircraft Corporation, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust; US access only)
Electroacoustic probe results obtained in an argon afterglow plasma for a planar geometry (Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1973), by Nicholas V. Karas and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
Flow regimes for hypervelocity vehicles (Wright-Patterson Air Force Base, Ohio : Directorate of Aeromechanics, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by Anthony Casaccio, Edgar Bendor, Republic Aviation Corporation, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
Electron reduction in the reentry plasma sheath (L.G. Hansom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force, 1969., 1969), by Daniel J. Jacavanco and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
Beryllium composite structures. Volume 1, Design and application (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by James N. Krusos, V. Rosa, R. E. Wiegert, F. B. Eck, T. T. Byrne, J. Borosic, A. S. Kjelby, Aeronca Aircraft Corporation, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
Re-entry vehicle control system design and mechanization (Wright-Patterson Air Force Base, Ohio: Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), by D. K. Scharmack, M. D. Ward, Air Force Flight Dynamics Laboratory (U.S.), and Honeywell Inc (page images at HathiTrust)
Laboratory and flight results of the microstrip plasma probe (Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1974), by Nicholas V. Karas and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
Performance of a microwave antenna system in the shoulder region of a blunt reentry nose cone (Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1973), by J. Leon Poirier, David H. Tropea, John D. Antonucci, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
A study of hypersonic aerodynamic drag devices : final technical report (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1960., 1960), by W. B. Champney, Wright Air Development Center, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
A preliminary report of human response to rearward-facing re-entry accelerations (Wright-Patterson Air Force Base, Ohio : Aero Medical Laboratory, Wright Air Development Center, Air Research and Development Command, U.S. Air Force, 1959., 1959), by Neville P. Clarke, Evan F. Lindberg, Neil S. Cherniack, A. S. Hyde, United States. Air Force. Air Research and Development Command, and Wright Air Development Center (page images at HathiTrust)
Design and testing of a chemical injection system for reentry plasma alleviation (Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1974), by John F. Lennon, Sheldon B. Herskovitz, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
Prediction of pressure fuctuations associated with maneuvering re-entry weapons. Volume 1 (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1977., 1977), by Anthony L. Laganelli, John R. Howe, Air Force Flight Dynamics Laboratory (U.S.), United States. Air Force. Systems Command, and General Electric Company. Re-entry and Environmental Systems Division (page images at HathiTrust)
Structural fabric and loom development : 21-foot wide airmat loom model GA-1 (Wright-Patterson Air Force Base, Ohio : Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), by D. M. Marco, J. O. Miller, Air Force Materials Laboratory (U.S.), Goodyear Aerospace Corporation, and United States. Air Force. Systems Command. Research and Technology Division (page images at HathiTrust)
An ablation technique for enhancing reentry antenna performance; flight test results (Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1974), by Dallas T. Hayes, J. Leon Poirier, John F. Lennon, Sheldon B. Herskovitz, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
Laminar heat transfer on sharp and blunt ten-degree cones in conical and parallel low-density flow (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), by David E. Boylan, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
Ablation modeling for dynamic simulation of reentry vehicles : preprint (Wright Patterson Air Force Base, Ohio : Air Vehicles Directorte, Air Force Research Laboratory, Air Force Materiel Command, 2006., 2006), by David B. Doman, William B. Blake, and Ohio). Air Vehicles Directorate Air Force Research Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
Catalytic surface recombination in boundary-layer profiles of the Falkner-Skan type (Washington, D.C. : Air Force Office of Scientific Research, United States Air Force, 1962., 1962), by William J. Rae, United States. Air Force. Office of Scientific Research, and Cornell Aeronautical Laboratory (page images at HathiTrust)
Investigation of the effects of nose bluntness on natural and induced boundary-layer transition on axisymmetric bodies in supersonic flow (Arnold Air Force Base, Tennessee : Von Kármán Gas Dynamics Facility, Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), by Jack D. Coats, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
Transient signal propagation in lossy plasmas (L.G. Hanscom Field, Massachusetts : Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1973., 1973), by Ronald L. Fante, Richard L. Taylor, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
A Study of aerodynamic effects of isothermal and temperature gradient atmospheres on reentry trajectories (Washington, D.C. : Air Force Office of Scientific Research, United States Air Force, 1962., 1962), by Leo Rute, United States. Air Force. Office of Scientific Research, and Polytechnic Institute of Brooklyn. Department of Aeronautical Engineering and Applied Mechanics (page images at HathiTrust)
Stability and transition analysis for reentry tool, STAR (Arlington, Virginia. : Air Force Office of Scientific Research, 2006., 2006), by Helen L. Reed, Texas A & M University. Aerospace Engineering Department, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Hypersonic dynamic stability Part II. Conical body experimental program (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967., 1967), by R. B. Hobbs, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and General Electric Company (page images at HathiTrust)
Trajectory generation using a modified simple shooting method (Wright Patterson Air Force Base, Ohio : Air Vehicles Directorte, Air Force Research Laboratory, Air Force Materiel Command, 2004., 2004), by Ashley Trent, David B. Doman, R. Venkataraman, Texas Tech University. Department of Mathematics, and Ohio). Air Vehicles Directorate Air Force Research Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
An algorithm for computing the range of trimable angle of attack for aircraft experiencing effector failures (Wright Patterson Air Force Base, Ohio : Air Vehicles Directorte, Air Force Research Laboratory, Air Force Materiel Command, 2002., 2002), by Joseph Kaloust, David B. Doman, Hope College, and Ohio). Air Vehicles Directorate Air Force Research Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
Hypersonic lifting body windward surface flow-field analysis for high angles of incidence (Arnold Air Force Base, Tennessee : Von Kármán Gas Dynamics Facility, Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), by John C. Adams, William R. Martindale, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
Finite difference schemes for the solution of the nosetip shape change equations (Los Angeles, California : Space and Missile Systems Organization, Los Angeles Air Force Station, Air Force Systems Command, United States Air Force, 1975., 1975), by P. G. Crowell, United States. Air Force. Systems Command, Space and Missile Systems Organization (U.S.), and Aerospace Corporation (page images at HathiTrust)
Interactions produced by sonic lateral jets located on surface in a supersonic stream (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), by W. T. Strike, J. S. Deitering, C. J. Schueler, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
Free-flight investigation of ablation effects n the stability of conical reentry configurations (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1972., 1972), by C. J. Welsh, G. L. Winchenbach, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
Dynamic inversion-based adaptive/reconfigurable control of the X-33 on ascent (Wright Patterson Air Force Base, Ohio : Air Vehicles Directorte, Air Force Research Laboratory, Air Force Materiel Command, 2002., 2002), by David B. Doman, Anhtuan D. Ngo, and Ohio). Air Vehicles Directorate Air Force Research Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
High altitude shock wave structure : Part 1 and Part 2 (Washington, D.C. : Air Force Office of Scientific Research, United States Air Force, 1962., 1962), by S. M. Scala, B. B. Cary, Lawrence Talbot, United States. Air Force. Office of Scientific Research, and General Electric Company. Space Sciences Laboratory (page images at HathiTrust)
Small vehicle dynamics study II : cross hatch studies (Norton Air Force Base, California : Space and Missile Systems Organization, Air Force Systems Command, United States Air Force, 1971., 1971), by Charles O. White, Henry L. Moody, Richard M. Grabow, United States. Air Force. Systems Command, Space and Missile Systems Organization (U.S.), and Philco-Ford Corporation (page images at HathiTrust)
Analysis of the three-dimensional compressible turbulent boundary layer on a sharp cone at incidence in supersonic and hypersonic flow (Arnold Air Force Base, Tennessee : Von Kármán Gas Dynamics Facility, Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1972., 1972), by John C. Adams, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
Laminar boundary-layer separation on flared bodies at supersonic and hypersonic speeds (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1965., 1965), by J. Don Gray, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
Nonequilibrium inviscid flow about blunt bodies (Inglewood, California : Space Systems Division, Air Force Systems Command, United States Air Force, 1964., 1964), by R. H. Lee, S. T. Chu, United States. Air Force. Systems Command. Space Systems Division, and Aerospace Corporation (page images at HathiTrust)
Neural dynamic trajectory design for reentry vehicles : preprint (Wright Patterson Air Force Base, Ohio : Air Vehicles Directorte, Air Force Research Laboratory, Air Force Materiel Command, 2007., 2007), by Ajay Verma, David B. Doman, Michael W. Oppenheimer, Daniel Schreiter, Rick Mayer, Kalyan Vadakkeveedu, Peng Xu, and Ohio). Air Vehicles Directorate Air Force Research Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
Hypersonic heat transfer measurements on re-entry vehivle surfaces at high Reynolds number (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory , Air Force Systems Command, United States Air Force, 1973., 1973), by Bryan E. Richards, United States. Air Force. Systems Command, Von Karman Institute for Fluid Dynamics, and Air Force Materials Laboratory (U.S.) (page images at HathiTrust)
Wall temperature effects on two- and three-dimensional transonic turbulent boundary layers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), by J. C Adams, Arloe W Mayne, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
A study of penetration of a liquid injectant into a supersonic flow (Los Angeles, California : Space and Missile Systems Organization, Los Angeles Air Force Station, Air Force Systems Command, United States Air Force, 1967., 1967), by Kenneth P. Horn, Roy E. Reichenbach, Marc A. Kolpin, United States. Air Force. Systems Command, Space and Missile Systems Organization (U.S.), and Aerospace Corporation (page images at HathiTrust)
Shock tunnel studies of high-enthalpy ionized airflows (Washington, D.C. : Air Force Office of Scientific Research, United States Air Force, 1962., 1962), by Alan Eschenroeder, A. Hertzberg, T. C. Golian, J. W. Daiber, United States. Air Force. Office of Scientific Research, and Cornell Aeronautical Laboratory (page images at HathiTrust)
Highly nonequilibrium boundary layer flows of a multicomponent dissociated gas mixture (Inglewood, California : Space Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), by G. I. Inger, United States. Air Force. Systems Command. Space Systems Division, and Aerospace Corporation (page images at HathiTrust)
Three-dimensional laminar boundary-layer analysis of upwash patterns and entrained vortex formation on sharp cones at angle of attack (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1971., 1971), by John C. Adams, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
Hypersonic dynamic stability. Part I. Summary (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967., 1967), by L. A. Marshall, United States. Air Force. Systems Command, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
Comparison of the effects of different transport coefficients on the nonlinear reflection and transmission coefficients of a reentry plasma (L.G. Hanscom Field, Massachusetts : Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1973., 1973), by Robert J. Papa, Richard L. Taylor, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
The calculation of lower bounds on the breakdown power levels of electromagnetic structures (L.G. Hanscom Field, Massachusetts : Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1973., 1973), by Dallas T. Hayes and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
Heat-transfer and shadowgraph tests of several elliptical lifting bodies at Mach 10 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), by M. E. Hillsamer, J. P. Rhudy, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
Investigation of landing point control of re-entry vehicles utilizing variable area aerodynamic decelerators incorporating lift (Wright-Patterson Air Force Base, Ohio : Flight Accessories Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by Avco-Everett Research Laboratory and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
Tests to determine subsonic pressures, forces and moments acting on a hypersonic re-entry configurations (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1963., 1963), by K. Mantz, R. Ross, D. B. Seager, United States. Air Force. Systems Command. Aeronautical Systems Division, Air Force Flight Dynamics Laboratory (U.S.), and Lockheed-California Company (page images at HathiTrust)
Dynamic stability of a system consisting of a stable parachute and an unstable load (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), by H. G. Heinrich, L. W. Rust, United States. Air Force. Systems Command. Research and Technology Division, Air Force Flight Dynamics Laboratory (U.S.), and University of Minnesota (page images at HathiTrust)
An investigation of hypersonic flow separation and control characteristics (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), by Louis G. Kaufman, Daniel Weiss, Stravos Hartofilis, Lawrence Meckler, United States. Air Force. Systems Command. Research and Technology Division, Air Force Flight Dynamics Laboratory (U.S.), and Grumman Aircraft Engineering Corporation (page images at HathiTrust)
Preliminary review of approximate calculative methods for transonic flow around bodies of revolution (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1972., 1972), by Jain-Ming Wu, Kinya Aoyama, Redstone Arsenal (Ala.), United States. Army. Missile Command, and University of Tennessee (System). Space Institute (page images at HathiTrust)
Experiments on the thermal performance of ribbon parachutes (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), by C. J. Scott, E. R. G. Eckert, United States. Air Force. Systems Command. Research and Technology Division, Air Force Flight Dynamics Laboratory (U.S.), and University of Minnesota. Department of Mechanical Engineering (page images at HathiTrust)

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