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Aerospace planes

See also what's at your library, or elsewhere.

• Hypersonic planes
• Reusable space vehicles

• Aero-space planes
• Planes, Aerospace
• Spaceplanes
• Transatmospheric aircraft

• NASP program authorization : hearing before the Subcommittee on Technology, Environment, and Aviation of the Committee on Science, Space, and Technology, U.S. House of Representatives, One Hundred Third Congress, first session, May 5, 1993. (Washington : U.S. G.P.O. : For sale by the U.S. G.P.O., Supt. of Docs., Congressional Sales Office, 1993), by Space United States. Congress. House. Committee on Science (page images at HathiTrust)
• Aerospace plane technology : research and development efforts in Japan and Australia : report to the Chairman, Committee on Science, Space, and Technology, House of Representatives / (Washington, D.C. : The Office ; Gaithersburg, MD (P.O. Box 6015, Gaithersburg 20877) : U.S. General Accounting Office [distributor, 1991]), by United States General Accounting Office and Space United States. Congress. House. Committee on Science (page images at HathiTrust)
• Study of a liquid metal NaK-77 for application in flight control systems., by R. C. Kumpitsch, P. J. Kroon, J. R. Granan, sponsor General Electric Company. Light Military Electronics Department, and issuing body United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Study of a liquid metal NaK-77 for application in flight control systems., by R. C. Kumpitsch, P. J. Kroon, J. R. Granan, sponsor General Electric Company. Light Military Electronics Department, sponsor Air Force Flight Dynamics Laboratory (U.S.), and issuing body United States. Air Force. Systems Command. Research and Technology Division (page images at HathiTrust)
• Fiber optics in aerospace vehicle hazard detection /, by Alan C. Traub (page images at HathiTrust)
• Optimum structural design concepts for aerospace vehicles : Bibliography and assessment /, by George Gerard, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor Allied Research Associates (page images at HathiTrust)
• Integrated hypersonic aerothermoelastic methodology for transatmospheric vehicle (TAV)/thermal protection system (TPS) structural design and optimization /, by D. D. Liu, Hilmi Kamhawl, Adel Chemaly, K. T. Chang, Lei Tang, P. C. Chen, and Ohio). Air Vehicles Directorate Air Force Research Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
• Non-linear effects in the longitudinal dynamics of a lifting vehicle in a circular orbit /, by R. S. Rangi, University of Toronto. Institute of Aerophysics. sponsor, and United States. Air Force. Office of Scientific Research. issuing body (page images at HathiTrust)

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

• Effect of forebody strakes on the aerodynamic characteristics in pitch and sideslip of a hypersonic airplane configuration at Mach numbers of 1.41, 2.01, and 6.86 / (Washington, D.C. : National Aeronautics and Space Administration, 1959), by Cornelius Driver and Langley Research Center (page images at HathiTrust)
• Preliminary survey of possible cooling methods for hypersonic aircraft / (Washington, D.C. : NACA, 1958), by Jack B. Esgar, Francis S. Stepka, Robert O. Hickel, United States. National Advisory Committee for Aeronautics, and Lewis Research Center (page images at HathiTrust)
• NASP program authorization : hearing before the Subcommittee on Technology, Environment, and Aviation of the Committee on Science, Space, and Technology, U.S. House of Representatives, One Hundred Third Congress, first session, May 5, 1993. (Washington : U.S. G.P.O. : For sale by the U.S. G.P.O., Supt. of Docs., Congressional Sales Office, 1993), by Space United States. Congress. House. Committee on Science (page images at HathiTrust)
• Evaluation of active cooling systems for a Mach 6 hypersonic transport airframe / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1971), by R. G. Helenbrook, F. M. Anthony, W. A. Mcconarty, Langley Research Center, and Bell Aerospace Company (page images at HathiTrust)
• Design of a convective cooling system for a Mach 6 hypersonic transport airframe / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1971), by R. G. Helenbrook, F. M. Anthony, Langley Research Center, and Bell Aerospace Company (page images at HathiTrust)
• A transonic wind-tunnel investigation of the static longitudinal and lateral aerodynamic characteristics of a proposed hypersonic glider with several booster configurations / (Washington [D.C.] : National Aeronautics and Space Administration, [1960]), by Ralph P. Bielat, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A feasibility study of heat-pipe-cooled leading edges for hypersonic cruise aircraft / (Washington, D.C. : National Aeronautics and Space Administration, 1971), by Calvin C. Silverstein, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Structural concepts for hydrogen-fueled hypersonic airplanes / (Washington, D.C. : National Aeronautics and Space Administration, [1966]), by L. Robert Jackson, Gregory R. Wichorek, John G. Davis, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Low-speed, high-lift aerodynamic characteristics of slender, hypersonic accelerator-type configurations / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1989), by Gregory M. Gatlin and Langley Research Center (page images at HathiTrust)
• The effects of wing plan form on the static longitudinal aerodynamic characteristics of a flat-top hypersonic aircraft at Mach numbers from 0.6 to 1.4 / (Washington [D.C.] : National Aeronautics and Space Administration, [1960]), by Stuart L. Treon, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An analytical study of hydrogen cooled panels for application to hypersonic aircraft / (Washington, D.C. : National Aeronautics and Space Administrtion, 1971), by W. G. Flieder, Langley Research Center, Garrett Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A method of solution with tabulated results for the attached oblique shock-wave system for surfaces at various angles of attack, sweep, and dihedral in an equilibrium real gas including the atmosphere / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1960), by Robert L. Trimpi, Robert A. Jones, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Theory and apparatus for measurement of emissivity for radiative cooling of hypersonic aircraft with data for inconel, iconel X, stainless steel 303, and titanium alloy RS-120 / (Washington, D.C. : U.S. G.P.O., 1961), by William J. O'Sullivan, William R. Wade, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Analysis of various descent trajectories for a hypersonic-cruise, cold-wall research airplane / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Pierce L. Lawing and Langley Research Center (page images at HathiTrust)
• Experimental low-speed and calculated high-speed aerodynamic characteristics of a hypersonic research airplane concept having a 65 ̊swept delta wing / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Jim A. Penland, Floyd G. Howard, Theodore R. Creel, and Langley Research Center (page images at HathiTrust)
• Flow field analysis of aircraft configurations using a numerical solution to the three-dimensional unified supersonic/hypersonic small disturbance equations / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1972), by R. C. Gunness, E. Dsylva, C. J. Knight, Langley Research Center, and Boeing Company (page images at HathiTrust)
• Local heat transfer and recovery temperatures on a yawed cylinder at a mach number of 4.15 and high Reynolds numbers, (Washington, G.P.O., 1961), by Ivan E. Beckwith and James J. Gallagher (page images at HathiTrust)
• Ground effects on the low-speed aerodynamics of a powered, generic hypersonic configuration / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1991), by Gregory M. Gatlin and Langley Research Center (page images at HathiTrust)
• Static stability characteristics of a series of hypersonic boost-glide configurations at mach numbers of 1.41 and 2.01 / (Washington [D.C.] : National Aeronautics and Space Administration, [1959]), by Gerald V. Foster and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Mechanics of a coned rotating net / ([Washington] : 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)
• Effects of body shape on the aerodynamic characteristics of an all-body hypersonic aircraft configuration at Mach numbers from 0.65 to 10.6 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by Walter P. Nelms and Ames Research Center (page images at HathiTrust)
• Experimental investigation of orthotropic panel flutter at arbitrary yaw angles, and comparison with theory / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1973), by Peter Shyprykevich, Langley Research Center, and Grumman Aerospace Corporation (page images at HathiTrust)
• The control of carbon dioxide cryodeposits / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Ellsworth L. Sharpe and Langley Research Center (page images at HathiTrust)
• Performance of a hypersonic hot fuselage structure with a carbon dioxide frost protected, nonintegral cryogenic tank / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Ellsworth L. Sharpe, L. Robert Jackson, and Langley Research Center (page images at HathiTrust)
• National Aero-Space Plane : a need for program direction and funding decisions : report to Congressional requesters / (Washington, D.C. : The Office ; Gaithersburg, MD (P.O. Box 6015, Gaithersburg 20884-6015) : The Office [distributor, 1993]), by United States General Accounting Office (page images at HathiTrust)
• Exploratory investigation of the effect of porous surfaces on hypersonic turbulent boundary layers / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1979), by Ralph D. Watson, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Recent advances in structures for hypersonic flight : proceedings of a symposium held at Langley Research Center, Hampton, Virginia, September 6-8, 1978. ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : for sale by the National Technical Information Service], 1978 [i.e. 1979]), by NASA Symposium on Recent Advances in Structures for Hypersonic Flight (1978 : Langley Research Center) (page images at HathiTrust)
• The National Aero-Space Plane : joint hearing before the Subcommittee on Transportation, Aviation, and Materials of the Committee on Science, Space, and Technology and the Subcommittee on Research and Development of the Committee on Armed Services, U.S. House of Representatives, One Hundred First Congress, first session, August 2, 1989. (Washington : U.S. G.P.O. : For sale by the Supt. of Docs., Congressional Sales Office, U.S. G.P.O., 1989), by Space United States. Congress. House. Committee on Science and United States. Congress. House. Committee on Armed Services. Subcommittee on Research and Development (page images at HathiTrust)
• NASP program authorization : hearing before the Committee on Science, Space, and Technology, U.S. House of Representatives, One Hundred Second Congress, second session, September 29, 1992. (Washington : U.S. G.P.O. : For sale by the U.S. G.P.O., Supt. of Docs., Congressional Sales Office, 1992), by Space United States. Congress. House. Committee on Science (page images at HathiTrust)
• Analysis of hypersonic pressure and heat transfer tests on delta wings with laminar and turbulent boundary layers / ([Washington, D.C.] : National Aeronautics and Space Administration, [1966]), by A. L. Nagel, L. B. Doyle, H. D. Fitzsimmons, and Langley Research Center (page images at HathiTrust)
• National Aerospace Plane (NASP) fiscal year 1991 RDT&E budget request : joint hearing before the Subcommittee of Transportation, Aviation and Materials of the Committee on Science, Space, and Technology, and the Subcommittee on Research and Development of the Committee on Armed Services, U.S. House of Representatives, One Hundred First Congress, second session, March 13, 1990. (Washington : U.S. G.P.O. : For sale by the Supt. of Docs., Congressional Sales Office, U.S. G.P.O., 1990), by Space United States. Congress. House. Committee on Science and United States. Congress. House. Committee on Armed Services. Subcommittee on Research and Development (page images at HathiTrust)
• Aerodynamic characteristics of a hypersonic transport configuration at Mach 6.86 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 20230], 1970), by William J. Small, David E. Fetterman, Frank S. Kirkham, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Sonic-boom characteristics of proposed supersonic and hypersonic airplanes / (Washington, D.C. : National Aeronautics and Space Administration, 1966), by F. Edward McLean, Lynn W. Hunton, Harry W. Carlson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Studies of airframe-propulsion-system integration for Mach 6 cruise vehicles / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by Frank S. Kirkham and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• An analytic study of radiatively cooled delta-wing structures for hypersonic aircraft / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1971), by James Campbell Robinson, George F. Klich, Robert R. McWithey, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Hypersonics before the shuttle : a concise history of the X-15 research airplane / (Washington, D.C. : National Aeronautics and Space Administration, NASA Office of Policy and Plans, NASA History Office, NASA Headquarters : For sale by the U.S. G.P.O., Supt. of Docs., [2000]), by Dennis R. Jenkins (page images at HathiTrust)
• Design and fabrication of a radiative actively cooled honeycomb sandwich structural panel for a hypersonic aircraft / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by D. A. Ellis, D. M. Schaeffer, L. L. Pagel, McDonnell Aircraft Company, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• High heat flux actively cooled honeycomb sandwich structural panel for a hypersonic aircraft / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by L. C. Koch, L. L. Pagel, Langley Research Center, McDonnell Douglas Corporation, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Assessment of flying-quality criteria for air-breathing aerospacecraft / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Duane T. McRuer, Dryden Flight Research Facility, and inc Systems Technology (page images at HathiTrust)
• Semiempirical method for predicting effects of incident-reflecting shocks on the turbulent boundary layer / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1965]), by S. Z. Pinckney and Langley Research Center (page images at HathiTrust)
• Effect of Reynolds number variation on aerodynamics of a hydrogen-fueled transport concept at Mach 6 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1987), by Jim A. Penland, Don C. Marcum, and Langley Research Center (page images at HathiTrust)
• Emittance, catalysis, and dynamic oxidation of Ti-14Al-21Nb / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1989), by K. E. Wiedemann, Sankara Narayan Sankaran, R. K. Clark, and Langley Research Center (page images at HathiTrust)
• Loading tests of a wing structure for a hypersonic aircraft / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by Roger A. Fields, William H. Siegel, Lawrence F. Reardon, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Determination of the effects of heating on modal characteristics of an aluminum plate with application to hypersonic vehicles / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1991), by H. Todd Snyder, M. W. Kehoe, and Dryden Flight Research Facility (page images at HathiTrust)
• An Inlet analysis for the NASA hypersonic research engine aerothermodynamic integration model / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Earl H. Andrews and Langley Research Center (page images at HathiTrust)
• Aerodynamic characteristics at Mach 6 of a hypersonic research airplane concept having a 70 ̊swept delta wing / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Louis E. Clark, Christine B. Richie, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aeordynamic characteristics of a distinct wing-body configuration at Mach 6 : experiment, theory, and the hypersonic isolation principle / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985), by Jim A. Penland, Jimmy L. Pittman, and Langley Research Center (page images at HathiTrust)
• Aerodynamic characteristics, including effect of body shape, of a Mach 6 aircraft concept / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983), by Gregory D. Riebe and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Fail-safe system for actively cooled supersonic and hypersonic aircraft / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Robert A. Jones, Christine B. Richie, Dorothy O. Braswell, and Langley Research Center (page images at HathiTrust)
• Ambient temperature fatigue tests of elements of an actively cooled honeycomb sandwich structural panel / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Ellsworth L. Sharpe, Wolf Elber, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Aerodynamic characteristics at Mach number 0.2 of a wing-body concept for a hypersonic research airplane / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by James L. Dillon, Theodore R. Creel, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Configuration heating for a hypersonic research airplane concept having a 70 ̊swept double-delta wing / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by Pierce L. Lawing and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Aerodynamic characteristics at Mach numbers from 0.33 to 1.20 of wing-body design concept for a hypersonic research airplane / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by James L. Dillon, Jimmy L. Pittman, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Optimum element density studies for finite-element thermal analysis of hypersonic aircraft structures / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, VA : For sale by the National Technical Information Service, 1990), by William L. Ko, Kyle M. Muramoto, Timothy Olona, and Dryden Flight Research Facility (page images at HathiTrust)
• Concept development of a Mach 4 high-speed civil transport / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by Christopher S. Domack and Langley Research Center (page images at HathiTrust)
• Hypersonic characteristics of an advanced aerospace plane at Mach 20.3 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1985), by Ronald S. McCandless and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 / ([Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by Jimmy L. Pittman, Gregory D. Riebe, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Flightweight radiantly and actively cooled panel : thermal and structural performance / (Washington, D.C. : National Aeronautics and Space Administation, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Charles P. Shore, H. Neale Kelly, Robert J. Nowak, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Internal convective cooling systems for hypersonic aircraft / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1975]), by Frank M. Anthony, Robert G. Helenbrook, W. H. Dukes, Langley Research Center, and Bell Aerospace Textron (page images at HathiTrust)
• Hypersonic cruise vehicle wing structure evaluation / (Washington, D.C. : National Aeronautics and Space Administration, 1970), by Kenneth A. Mason, P. P. Plank, United States National Aeronautics and Space Administration, Langley Research Center, and Lockheed Missiles and Space Company (page images at HathiTrust)
• Validation of scramjet exhaust simulation technique at Mach 6 / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1979), by H. B. Hopkins, J. Leng, W. Konopka, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Hypersonic airframe structures technology needs and flight test requirements / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by National Technical Information Service], 1979), by J. E. Stone, McDonnell Douglas Corporation, Langley Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and L. C. Koch (page images at HathiTrust)
• Investigation of the aerodynamic characteristics of a hypersonic transport model at Mach numbers to 6 / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1971), by James C. Ellison, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Turbojet-ramjet propulsion system for all-body hypersonic aircraft [electronic resource] / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 20230], 1971), by Mark H. Waters and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic characteristics of an all-body hypersonic aircraft configuration at Mach numbers from 0.65 to 10.6 / (Washington : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1971), by Walter P. Nelms, Charles L. Thomas, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The static stability characteristics of several preliminary models of the X-15 research airplane at Mach numbers of 2.98 and 4.01 / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by Robert W. Dunning, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Control integration concept for hypersonic cruise-turn maneuvers / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by David L. Raney, Frederick J. Lallman, and Langley Research Center (page images at HathiTrust)
• Combined compressive and shear buckling analysis of hypersonic aircraft structural sandwich panels / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1991), by William L. Ko, Raymond H. Jackson, and Dryden Flight Research Facility (page images at HathiTrust)
• Aerodynamic characteristics of two single-stage-to-orbit vehicles at Mach 20.3 / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Peter T. Bernot and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Mach 4 free-jet tunnel-starting experiments for a hypersonic research engine model causing high blockage / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by George T. Carson, Raymond E. Midden, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic characteristics at Mach 6 of a wing-body concept for a hypersonic research airplane / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by James L. Dillon, Jimmy L. Pittman, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach number 0.2 / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by Jim A. Penland, James L. Dillon, Theodore R. Creel, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Aerodynamic characteristics at Mach numbers of 1.5, 1.8, and 2.0 of a blended wing-body configuration with and without integral canards / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Office, 1979), by A. Warner Robins, David S. Miller, Milton Lamb, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Langley Research Center (page images at HathiTrust)
• Analysis of hypersonic pressure and heat transfer tests on a flat plate with a flap and a delta wing with body, elevons, fins, and rudders / ([Washington] : National Aeronautics and Space Administration : For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1966), by H. L. Giles, J. W. Thomas, and Langley Research Center (page images at HathiTrust)
• A methodology for boost-glide transport technology planning / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by E. M. Repic, R. J. Milliken, G. A. Olson, Langley Research Center, and Rockwell International. Space Division (page images at HathiTrust)
• Validation of scramjet exhaust simulation technique / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by H. B. Hopkins, J. Leng, H. B. Konopka, United States National Aeronautics and Space Administration, Langley Research Center, and Grumman Aerospace Corporation (page images at HathiTrust)
• A fuselage/tank structure study for actively cooled hypersonic cruise vehicles--summary / (Washington : U.S. National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by C. J. Pirrello, J. E. Stone, A. H. Baker, McDonnell Douglas Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Study of a fail-safe abort system for an actively cooled hypersonic aircraft : volume I--technical summary / (Washington : U.S. National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by C. J. Pirrello, R. L. Herring, United States National Aeronautics and Space Administration, McDonnell Douglas Corporation, and Langley Research Center (page images at HathiTrust)
• CAVE : a computer code for two-dimensional transient heating analysis of conceptual thermal protection systems for hypersonic vehicles / ([Washington] : National Aeronautics and Space Administration : Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Kenneth A. Rathjen and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Thermal design for areas of interference heating on actively cooled hypersonic aircraft / (Washington : National Aeronautics and Space Administration, Scientific and Technical Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by R. L. Herring, J. E. Stone, McDonnell Douglas Corporation, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Development and validation of purged thermal protection systems for liquid hydrogen fuel tanks of hypersonic vehicles / (Washington : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1977), by R. G. Helenbrook, J. Z. Colt, Bell Aerospace Company, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Method for obtaining aerodynamic data on hypersonic configurations with scramjet exhaust flow simulation / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by William R. Hartill and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Actively cooled plate fin sandwich structural panels for hypersonic aircraft / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1979), by L. M. Smith, C. S. Beuyukian, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Exploratory study of open-face honeycomb to reduce temperature of hypersonic aircraft structure / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 20230], 1969), by L. Roane Hunt, R. R. Howell, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Turbulent-skin-friction and heat-transfer charts adapted from the Spalding and Chi method / (Washington, D. C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by Luther Neal, Mitchel H. Bertram, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Interference effects of canard controls on the longitudinal aerodynamic characteristics of a winged body at Mach 10 / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1968), by Cuyler W. Brooks, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of two-dimensional multiple sine-wave protrusions on the pressure and heat-transfer distributions for a flat plate at Mach 6 / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1968]), by Aubrey M. Cary, E. Leon Morrisette, and Langley Research Center (page images at HathiTrust)
• Scramjet nozzle design and analysis as applied to a highly integrated hypersonic research airplane / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by William J. Small, P. J. Johnston, John P. Weidner, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of effect of propulsion system installation and operation on aerodynamics of an airbreathing hypersonic airplane at Mach O.3 to 1.2 / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by James M. Cubbage, Charles E. Mercer, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental performance of an ablative material as an external insulator for a hpersonic research aircraft / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Richard L. Puster, Andrew J. Chapman, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerothermal and structural performance of a cobalt-base superalloy thermal protection system at Mach 6.6 / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by James Wayne Sawyer, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Downstream influence of swept slot injection in hypersonic turbulent flow / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Jerry N. Hefner, Dennis M. Bushnell, Aubrey M. Carey, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Flutter design of stiffened-skin panels for hypersonic aircraft / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Herman L. Bohon, Walter L. Heard, Melvin S. Anderson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A forebody design technique for highly integrated botton-mounted scramjets with application to a hypersonic research airplane / (Washington : National Aeronautics and Space Administration : Springfield, Va. : For sale by the National Technical Information Service, 1976), by C. L. W. Edwards and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Electron attachment to atomic fluorine in thermally ionized air / (Washington, D.C. : National Aeronautics and Space Administration, 1966), by Robert Earl Good (page images at HathiTrust; US access only)
• National Aerospace Plane (NASP) fiscal year 1992 RDT&E budget request : joint hearing before the Subcommittee on Technology and Competitiveness of the Committee on Science, Space, and Technology and the Subcommittee on Research and Development of the Committee on Armed Services, U.S. House of Representatives, One Hundred Second Congress, first session, March 12, 1991. (Washington : U.S. G.P.O. : For sale by Supt. of Docs., Congressional Sales Office, U.S. G.P.O., 1991), by Space United States. Congress. House. Committee on Science and United States. Congress. House. Committee on Armed Services. Subcommittee on Research and Development (page images at HathiTrust)
• Telemeter transmission at 219.5 megacycles from two rocket-powered models at Mach number up to 15.7 / (Washington, D.C. : National Advisory Committee for Aeronautics, 1958), by George B. Graves, J. Thomas Markley, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• The Hypersonic revolution : eight case studies in the history of hypersonic technology : a Special Staff Office study / (Wright-Patterson Air Force Base, Ohio : Special Staff Office, Aeronautical Systems Division, Wright-Patterson Air Force Base, 1987), by Richard Hallion and United States. Air Force. Systems Command. Aeronautical Systems Division. Special Staff Office (page images at HathiTrust)
• Lift, drag, and static longitudinal stability data from an exploratory investigation at a Mach number of 6.86 of an airplane configuration having a wing of trapezoidal plan form / (Washington, D.C. : National Advisory Committee for Aeronautics, 1955), by Jim A. Penland, David E. Fetterman, Herbert W. Ridyard, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Experimental results of cooling a 12.5 ̊semivertex angle cone by ejection of hydrogen and helium from its apex at Mach 7 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1964), by George F. Klich, Edward W. Leyhe, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Investigation of dynamic stability derivatives of vehicles flying at hypersonic velocity /, by Arthur Gilmore, Donald Mackenzie, Vladimir Seredinsky, issuing agency United States. Air Force. Systems Command. Aeronautical Systems Division, and sponsor Grumman Aircraft Engineering Corporation (page images at HathiTrust)
• An experimental and analytical investigation of hypersonic inlet boundary layers /, by J. F. Stroud, L. D. Miller, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Lockheed-California Company (page images at HathiTrust)
• The analytical determination of the thermal response of a typical aircraft structure subjected to transient external heating and cooling /, by Thomas N. Bernstein, Robert M. Engle, Gene E. Maddux, and sponsor Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• National Aerospace Plane (NASP) fiscal year 1991 RDT & E budget request : joint hearing before the Subcommittee on Transportation, Aviation, and Materials of the Committee on Science, Space, and Technology and the Subcommittee on Research and Development of the Committee on Armed Services, U.S. House of Representatives, One Hundred First Congress, second session, March 13, 1990. (Washington : U.S. G.P.O. : For Sale by the Supt. of Docs., Congressional Sales Office, U.S. G.P.O., 1990), by Space United States. Congress. House. Committee on Science and United States. Congress. House. Committee on Armed Services. Subcommittee on Research and Development (page images at HathiTrust)
• Determination of factors governing selection and application of materials for ablation cooling of hypervelocity vehicles /, by John H. Bonin, Donald E. Taylor, Channon F. Price, issuing body Wright Air Development Center, and sponsor United States. Air Force. Air Research and Development Command (page images at HathiTrust; US access only)
• Integrated hypersonic aerothermoelastic methodology for transatmospheric vehicle (TAV)/thermal protection system (TPS) structural design and optimization /, by D. D. Liu, Hilmi Kamhawl, Adel Chemaly, K. T. Chang, Lei Tang, P. C. Chen, and Ohio). Air Vehicles Directorate Air Force Research Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
• A flexible hypersonic vehicle model developed with piston theory : preprint /, by Michael W. Oppenheimer, David B. Doman, and Ohio). Air Vehicles Directorate Air Force Research Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
• Trajectory generation using a modified simple shooting method /, by Ashley Trent, David B. Doman, R. Venkataraman, sponsor Texas Tech University. Department of Mathematics, and Ohio). Air Vehicles Directorate Air Force Research Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
• Output feedback control and sensor placement for a hypersonic vehicle model : preprint /, by Pete Jankovsky, David B. Doman, Michael A. Bolender, Stephan Yurkovich, Andrea Serrani, David O. Sigthorsson, sponsor Ohio State University. Department of Electrical and Computer Engineering, and Ohio). Air Vehicles Directorate Air Force Research Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
• Hypersonic maneuvering vehicle simulations using real-aas, unstructured Navier-Stokes software /, by William D. McGrory, Inc. AeroSoft, and issuing body United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Free flight hypersonic heat transfer and boundary layer transition studies: HTV flights A-40 and A-41 /, by James E. Brunk, Warren N. White, issuing body Aerospace Research Laboratories (U.S.), and sponsor Curtiss-Wright Corporation (page images at HathiTrust)
• Low-density flow effects for hypervelocity vehicles : phase II /, by Roop N. Gupta, Sudheer N. Nayani, Inc. ViGYAN, sponsor Wright Research and Development Center, sponsor Air Force Flight Dynamics Laboratory (U.S.), and issuing body United States. Air Force. Systems Command (page images at HathiTrust)

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