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Lunar excursion module -- Design and construction

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• Lunar excursion module
• Space vehicles -- Design and construction
• Design and construction

• Apollo experience report : lunar module structural subsystem (National Aeronautics and Space Administration ;, 1973), by Stanley P. Weiss and Manned Spacecraft Center (U.S.) (page images at HathiTrust)

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

• Mission report, Apollo 10. (For sale by Supt. of Docs., U. S. Govt. Print. Off.], 1969), by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Apollo experience report : guidance and control systems : lunar module mission programer (National Aeronautics and Space Administration, 1975), by Jesse A. Vernon and Lyndon B. Johnson Space Center (page images at HathiTrust)
• Apollo experience report : guidance and control systems : lunar module abort guidance system (National Aeronautics and Space Administration ;, 1975), by Pat M. Kurten and Lyndon B. Johnson Space Center (page images at HathiTrust)
• Scaled lunar module jet erosion experiments (National Aeronautics and Space Administration ;, 1969), by Norman S. Land and Harland F. Scholl (page images at HathiTrust)
• NASA TN D-6719 (National Aeronautics and Space Administration :, 1972), by Michael J. Rutkowski, Manned Spacecraft Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Apollo experience report : descent propulsion system (National Aeronautics and Space Administration ;, 1973), by William R. Hammock, Arlie E. Fisher, Eldon C. Currie, and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
• NASA TN D-6724 (National Aeronautics and Space Administration :, 1972), by Richard J. Gillen, Frank Collier, James C. Brady, Manned Spacecraft Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6725 (National Aeronautics and Space Administration :, 1972), by Claude A. Graves, Jon C. Harpold, Manned Spacecraft Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental determination of potential lunar surface organic contamination in the lunar module descent-engine exhaust (National Aeronautics and Space Administration ;, 1972), by D. A. Flory and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
• Preliminary investigation of the handling qualities of a vehicle in a simulated lunar gravitational field (National Aeronautics and Space Administration :, 1965), by Peter C. Boisseau and Langley Research Center (page images at HathiTrust)
• Apollo experience report : lunar module instrumentation subsystem (National Aeronautics and Space Administration ;, 1972), by David E. O'Brien, Jared R. Woodfill, and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
• Apollo experience report : mission planning for lunar module descent and ascent (National Aeronautics and Space Administration ;, 1972), by Floyd V. Bennett and Manned Spacecraft Center (U.S.) (page images at HathiTrust)

• NASA TN D-4474 (National Aeronautics and Space Administration ;, 1968), by Ulysse J. Blanchard, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)

• Performance analysis of the ascent propulsion system of the Apollo spacecraft (National Aeronautics and Space Administration ;, 1973), by John C. Hooper and Lyndon B. Johnson Space Center (page images at HathiTrust)

• The determination of the helium saturation level of Aerozine-50 and nitrogen tetroxide (National Aeronautics and Space Administration ;, 1971), by Irwin D. Smith, Richard P. Schroats, and Manned Spacecraft Center (U.S.) (page images at HathiTrust)

• Lunar landing and site selection study (National Aeronautics and Space Administration ;, 1965), by James L. Lewis, Charles D. Wheelwright, and Manned Spacecraft Center (U.S.) (page images at HathiTrust)

• NASA TN D-4474 (National Aeronautics and Space Administration ;, 1968), by Ulysse J. Blanchard, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-4089 (National Aeronautics and Space Administration ;, 1967), by G. Kimball Miller, L. Keith Barker, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)

• Full-scale dynamic landing-impact investigation of a prototype lunar module landing gear (National Aeronautics and Space Administration ;, 1969), by Ulysse J. Blanchard, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)

• Analysis of maximum range trajectories for rocket-propelled lunar flying vehicles in a uniform gravitational field (National Aeronautics and Space Administration ;, 1969), by A. Gary Childs, Ernest S. Armstrong, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• A mathematical procedure for predicting the touchdown dynamics of a soft-landing vehicle (National Aeronautics and Space Administration ;, 1971), by George A. Zupp, Harold H. Doiron, and Manned Spacecraft Center (U.S.) (page images at HathiTrust)

• NASA TN D-4680 (National Aeronautics and Space Administration ;, 1968), by Robert W. Herr, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)

• NASA TN D-3972 (National Aeronautics and Space Administration ;, 1967), by Howard G. Hatch, Jere B. Cobb, Jack E. Pennington, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)

• Anthropometric source book ([Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Office, 1978., 1978), by Anthropology Research Project (Webb Associates) (page images at HathiTrust)
• Basic science for aerospace vehicles. (McGraw, 1963), by Northrop Institute of Technology and James L. McKinley (page images at HathiTrust)
• Aerospace vehicle design. (Johnson Pub. Co., 1963), by K. D. Wood (page images at HathiTrust)
• Human spaceflight : the space shuttle and beyond : hearing before the Subcommittee on Science and Space of the Committee on Commerce, Science, and Transportation, United States Senate, One Hundred Ninth Congress, first session, May 18, 2005. (U.S. G.P.O. :, 2006), by Science United States. Congress. Senate. Committee on Commerce (page images at HathiTrust)
• Development of the Crew Exploration Vehicle (U.S. G.P.O. :, 2007), by United States. Congress. House. Committee on Science (page images at HathiTrust)
• A study in computer aided aerospace vehicle design (Naval Undersea Research and Development Center, 1969), by Dale Eugene Calkins and Naval Undersea Research and Development Center (page images at HathiTrust)
• Structural interaction with control systems. (National Aeronautics and Space Administration;, 1971), by R. B. Noll and J. Zvara (page images at HathiTrust)
• Solid propellant selection and characterization. (National Aeronautics and Space Administration; [for sale by the National Technical Information Service, Springfield, Va.], 1971), by Thomas N. Scortia and Howard G. Cutforth (page images at HathiTrust)
• Space vehicle displays design criteria. (National Aeronautics and Space Administration;, 1972), by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Preliminary criteria for the fracture control of space shuttle structures. (National Aeronautics and Space Administration;, 1971), by Hampton United States. Langley Research Center and McDonnell Douglas Astronautics Company. Design Criteria Program Office (page images at HathiTrust)
• Effects of structural flexibility on entry vehicle control systems. [Prepared for NASA under the cognizance of the Jet Propulsion Laboratory, California Institute of Technology. (National Aeronautics and Space Administraiton;, 1972), by John J. Deyst, R. B. Noll, Jet Propulsion Laboratory (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Combining ascent loads. (National Aeronautics and Space Administration;, 1972), by John Cornelius Houbolt (page images at HathiTrust)
• Structural interaction with transportation and handling systems (National Aeronautics and Space Administration, 1973), by F. L. Rish, L. Kovalevsky, and R. Weldon (page images at HathiTrust)
• Structural design criteria applicable to a space shuttle. (National Aeronautics and Space Administration, 1972), by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Mechanical design of spacecraft; seminar proceedings, March 28-MAY 23, 1962. (Jet Propulsion Laboratory, California Institute of Technology, 1962), by Jet Propulsion Laboratory (U.S.) (page images at HathiTrust)
• Proceedings. (Jet Propulsion Laboratory, California Institute of Technology, 1970), by University of Santa Clara Aerospace Mechanisms Symposium. 4th, Mary Fran Buehler, and George D. Herzl (page images at HathiTrust)
• Proceedings of the 3rd Aerospace Mechanisms Symposium, held at the Jet Propulsion Laboratory, Pasadena, California, May 23-24, 1968. (Jet Propulsion Laboratory, California Institute of Technology, 1968), by Aerospace Mechanisms Symposium (3rd : 1968 : Jet Propulsion Laboratory), Jet Propulsion Laboratory (U.S.), Lockheed Missiles and Space Company, and University of Santa Clara (page images at HathiTrust)
• Thermoelectric Outer Planets Spacecraft (TOPS) Advanced Systems Technology Project; final report. (Jet Propulsion Laboratory, California Institute of Technology, 1973), by California Institute of Technology. Thermoelectric Outer Planets Spacecraft Project and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Structural design of missiles and spacecraft (McGraw-Hill, 1962), by Lewis H Abraham (page images at HathiTrust)
• Mars sample return mission : 1985 study report (JPL, California Institute of Technology :, 1986), by James R French, Douglas P Blanchard, Jet Propulsion Laboratory (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Mars sample return mission : 1984 study report (JPL, California Institute of Technology :, 1984), by J. Pieter de Vries, Douglas P Blanchard, Harry N Norton, Jet Propulsion Laboratory (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Spacecraft systems (Scientific and Technical Information Division, National Aeronautics and Space Administration; [for sale by the Superintendent of Documents, U.S. Govt. Print. Off.], 1965), by Lewis H. Abraham (page images at HathiTrust)
• Probabilistic risk analysis of flying the space shuttle with and without fuel turbine discharge temperature redline protection (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987), by Leonard W. Howell, George C. Marshall Space Flight Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Practices in adequate structural design (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989), by Robert S. Ryan and George C. Marshall Space Flight Center (page images at HathiTrust; US access only)
• Terrestrial environment (climatic) criteria guidelines for use in aerospace vehicle development : 1977 revision (National Aeronautics and Space Administration ;, 1977), by John W. Kaufman and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Automated Mars surface sample return mission concepts for achievement of essential scientific objectives (National Aeronautics and Space Administration ;, 1975), by William L. Weaver, Wayne L. Darnell, Harry N. Norton, and Langley Research Center (page images at HathiTrust)
• Jupiter probe charging study (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by Carolyn K. Purvis, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Lewis Research Center (page images at HathiTrust)
• Vibration characteristics of a steadily rotating slender ring (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by Frederick J. Lallman, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Tests of graphite/polymide sandwich panels in uniaxial edgewise compression (National Aeronautics and Space Administration, Scientific and Technical Information Branch;, 1980), by Charles J. Camarda, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Asymmetric nonlinear dynamic response and buckling of shallow spherical shells (National Aeronautics and Space Administration ;, 1969), by Atis A. Liepens, Dynatech Corporation, and Langley Research Center (page images at HathiTrust)
• Electrolysis cell for orbital test (National Aeronautics and Space Administration ;, 1966), by C. W. Fetheroff, TRW Incorporated, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Some considerations in the fatigue design of launch and spacecraft structures (National Aeronautics and Space Administration ;, 1965), by R. H. Christensen, R. J. Bellinfante, and Douglas Aircraft Company (page images at HathiTrust)
• Engine operating problems in space : the space environment (National Aeronautics and Space Administration, 1965), by D. Christensen (page images at HathiTrust; US access only)
• Geometrical and inertial properties of a class of thin shells of a general type (National Aeronautics and Space Administration, 1965), by Will J. Worley and Han-chung Wang (page images at HathiTrust; US access only)
• Transfer function approximations for large highly coupled elastic boosters with fuel slosh (National Aeronautics and Space Administration, 1966), by R. L. Stapleford (page images at HathiTrust; US access only)
• Viking dynamics experience with application to future payload design (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Stanley Barrett, Kenneth R. Payne, W. Paul Rader, Langley Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Martin Marietta Corporation (page images at HathiTrust)
• Assessment of space vehicle aeroacoustic- vibration prediction, design, and testing (National Aeronautics and Space Administration ;, 1970), by Harry Himelblau, Terry D. Scharton, C. Myron Fuller, Langley Research Center, and McDonnell Douglas Astronautics Company-West (page images at HathiTrust)
• Critical requirements for the design of large space structures (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by John M. Hedgepeth, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• NASA TN D-1981 (National Aeronautics and Space Administration ; [For sale by the Technical Services, Department of Commerce, Washington, D.C. 20230], 1964), by C. Robert Nysmith, B. Pat Denardo, James L. Summers, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Apollo experience report : crew station integration. (National Aeronautics and Space Administration ;, 1973), by Charles D. Wheelwright, Marion W. Hix, Frank E. Wittler, William A. Langdoc, Dale A. Nussman, Louis D. Allen, and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
• NASA TN D-3745 (National Aeronautics and Space Administration :, 1966), by Wayne R. Hudson, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-4074 (National Aeronautics and Space Administration ;, 1967), by William E. Lang, George H. Honeycutt, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A central facility for recording and processing transient-type data (National Aeronautics and Space Administration :, 1963), by Staff : Lewis Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-4066 (National Aeronautics and Space Administration ;, 1967), by William J. Masica, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Apollo experience report--crew station integration : volume I-- crew station design and development (U.S. National Aeronautics and Space Administration ;, 1976), by Louis D. Allen, Dale A. Nussman, and Lyndon B. Johnson Space Center (page images at HathiTrust)
• NASA TN D-6039 (National Aeronautics and Space Administration ;, 1970), by C. Robert Nysmith, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5943 (National Aeronautics and Space Administration :, 1970), by Robert R. Clary, Lloyd J. Turner, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-4688 (National Aeronautics and Space Administration ;, 1968), by William C. Moseley, Jack E. Hughes, Ralph E. Graham, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5910 (National Aeronautics and Space Administration :, 1970), by Doyle P. Swofford, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5919 (National Aeronautics and Space Administration :, 1970), by Douglas A. Anderson, Lewis 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)
• NASA TN D-6656 (National Aeronautics and Space Administration :, 1972), by Irving Abel, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6724 (National Aeronautics and Space Administration :, 1972), by Richard J. Gillen, Frank Collier, James C. Brady, Manned Spacecraft Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-4598 (National Aeronautics and Space Administration ;, 1968), by George C. Ashby, W. Frank Staylor, Langley Research Center, and United States National Aeronautics and Space Administration (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)
• NASA TN D-1861 (National Aeronautics and Space Administration :, 1964), by Gregory R. Wichorek, Bland A. Stein, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Conversion of a spacecraft designed for manned space flight to a recoverable orbiting astronomical observatory (National Aeronautics and Space Administration :, 1964), by Windsor L. Sherman and Langley Research Center (page images at HathiTrust)
• NASA TN D-4563 (National Aeronautics and Space Administration ;, 1968), by Jerry C. South, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-1692 (National Aeronautics and Space Administration, 1962), by H. U. Schuerch, A. C. Kyser, O. R. Burggraf, Astro Research Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-1714 (National Aeronautics and Space Administration, 1963), by W. B. Fussell, F. A. Jerozal, J. J. Triolo, Inc Continental Technical Service, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Application of the stored-program computer to small scientific spacecraft (National Aeronautics and Space Administration ;, 1967), by Rodger A. Cliff, United States National Aeronautics and Space Administration, and Goddard Space Flight Center (page images at HathiTrust)
• Orbit-launched nuclear vehicle design and performance evaluation procedure for escape and planetary missions (National Aeronautics and Space Administration, 1963), by Ronald J. Harris, United States National Aeronautics and Space Administration, and Robert E. Austin (page images at HathiTrust)
• NASA TN D-1675 (National Aeronautics and Space Administration, 1963), by Carl E. Fichtel, K. W. Ogilvie, D. A. Kniffen, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-3489 (National Aeronautics and Space Administration :, 1966), by Dale W. Harris, J. J. Ketchman, R. J. Burian, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6349 (National Aeronautics and Space Administration ;, 1971), by Willie Heineman, Manned Spacecraft Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-6140 (National Aeronautics and Space Administration ;, 1971), by L. David Wall, Michael F. Card, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6133 (National Aeronautics and Space Administration :, 1971), by Paul A. Cooper, Martha P. Robinson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Apollo experience report : spacecraft structure subsystem (National Aeronautics and Space Administration, 1974), by P. D. Smith and Lyndon B. Johnson Space Center (page images at HathiTrust)
• Effect of temperature on radiator weight for space vehicle power plants (Oak Ridge National Laboratory, 1960), by P. G. Lafyatis, Oak Ridge National Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Flight test results pertaining to the Space Shuttlecraft : a symposium held at Flight Research Center, Edwards, Calif., June 30, 1970. (National Aeronautics and Space Administration ;, 1970), by Flight Research Center (U.S.) (page images at HathiTrust)
• An investigation at subsonic speeds of the longitudinal aerodynamic characteristics at angles of attach from -4° to 100° of delta-wing reentry configurations having vertically displaced and cambered wing-tip panels (National Aeronautics and Space Administration, 1961), by Bernard Spencer and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Meteoroid hazard to space vehicles in orbit near the earth : a functional interpretation of the information for design and operations decisions (National Aeronautics and Space Administration ;, 1962), by Charles C. Dalton, United States National Aeronautics and Space Administration, and George C. Marshall Space Flight Center (page images at HathiTrust)
• Extreme temperature range organic coolants. (Wright Air Development Division, Air Research and Development Command, U. S. Air Force, 1961), by Dale A. Barsness (page images at HathiTrust)
• Saturn V flight manual, SA 504. (The Center, 1969), by George C. Marshall Space Flight Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Saturn V flight manual, SA 507. ([Huntsville?], 1969), by George C. Marshall Space Flight Center (page images at HathiTrust)
• Structures for space operations. (National Aeronautics and Space Adminstration, Office of Scientific and Technical Information; [for sale by the Superintendent of Documents, U.S. Govt. Print. Off.], 1963), by NASA-University Conference on the Science and Technology of Space Exploration (1962 : Chicago) (page images at HathiTrust; US access only)
• Path from low earth orbit to Mars ([publisher not identified], 2013), by United States Senate Committee on Commerce, Science, and Transportation (page images at HathiTrust)
• Composite construction for flight vehicles : [with list of referenced documents.]. ([Washington, D.C.], 1960), by United States Department of Defense (page images at HathiTrust)
• Approximate transfer functions for flexible-booster-and-autopilot analysis (Wright-Patterson Air Force Base, Ohio : Flight Control Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), by David R. Lukens, George T. Broucek, ALfred F. Schmitt, United States. Air Force. Air Research and Development Command, and Wright Air Development Division (page images at HathiTrust)
• Development of procedures for large scale automated minimum weight structural design (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 Ronald A. Gellatly, Bell Aerospace Textron, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Design techniques for flight control systems in nuclear radiation environments (Wright-Patterson Air Force Base, Ohio : Flight Control Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), by R. M. Magee, D. B. Taulbee, S. I. Rosen, G. M. Brown, United States. Air Force. Systems Command. Aeronautical Systems Division, United States. Air Force. Systems Command. Aeronautical Systems Division. Directorate of Materials and Processesd States, and Bendix Corporation (page images at HathiTrust)
• Multiwall structures for space vehicles (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Air Research and Development Command, U.S. Air Force, 1960., 1960), by S. Lampert, Dewey G. Younger, United States. Air Force. Air Research and Development Command, United States. Wright Air Development Division, and Aeronutronic Ford Corporation (page images at HathiTrust)
• Robustness improvement of actively controlled structures through integrated structural/control design (Wright-Patterson Air Force Base, Ohio : Fliight Dynamics Directorate, Wright Laboratory, Air Force Systems Command, 1991, 1991), by S. S. Rao, T. S. Pan, Ohio) Wright Laboratory (Wright-Patterson Air Force Base, and Purdue University. School of Mechanical Engineering (page images at HathiTrust)
• Long duration exposure facility mini-data base user's guide : IBM-compatible PC computer version (National Aeronautics and Space Administration, Langley Research Center, 1995), by G. L. Bohnhoff-Hlavacek, H. W. Dursch, H. Gary Pippin, and Langley Research Center (page images at HathiTrust)
• Long duration exposure facility mini-data base user's guide : Macintosh version (National Aeronautics and Space Administration, Langley Research Center, 1995), by G. L. Bohnhoff-Hlavacek, H. W. Dursch, H. Gary Pippin, and Langley Research Center (page images at HathiTrust)
• Solid rocket motor igniters. (National Aeronautics and Space Administration;, 1971), by Donald H. Barrett (page images at HathiTrust)
• Large space systems technology, 1979 : first annual program technical review held at NASA Langley Research Center, Hampton, Virginia, November 7-8, 1979 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by J. C. Ward and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)

More items available under broader and related terms at left.