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Stability of space vehicles -- Equipment and supplies

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• Stability of space vehicles
• Space vehicles -- Equipment and supplies
• Equipment and supplies

• Stability of space vehicles -- Measurement -- Equipment and supplies

• The annular momentum control device (AMCD) and potential applications (National Aeronautics and Space Administration ;, 1975), by Willard W. Anderson, Nelson J. Groom, and Langley Research Center (page images at HathiTrust)

• Vehicle attitude determination with a single onboard camera (National Aeronautics and Space Administration ;, 1968), by Richard J. Bendura, Robert E. Smith, Allen B. Henning, and Langley Research Center (page images at HathiTrust)

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

• 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)
• Effects of relaxed static longitudinal stability on a single-stage-to-orbit vehicle design (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Delma C. Freeman, Alan W. Wilhite, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Analysis of random signal combinations for spacecraft pointing stability (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by Leonard W. Howell and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Subsonic and transonic dynamic-stability characteristics of the space shuttle launch vehicle (U.S. National Aeronautics and Space Administration ;, 1976), by Delma C. Freeman, Edwin E. Davenport, Richmond P. Boyden, and Langley Research Center (page images at HathiTrust)
• Effect of Reynolds number on the aerodynamic stability and control characteristics of a 55 ̊clipped-delta-wing orbiter configuration at supersonic mach numbers (U.S. National Aeronautics and Space Administration ;, 1976), by A. B. Blair, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Effect of modifications on aerodynamic characteristics of a single-stage-to-orbit vehicle at Mach 5.9 (U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by Peter T. Bernot, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Static and dynamic stability analysis of the Space Shuttle Vehicle-Orbiter (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Wei J. Chyu, Larry L. Erickson, Ralph K. Cavin, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• The N-BOD₂ user's and program's manual (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Harold P. Frisch and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Comparison of space shuttle orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by Delma C. Freeman, Bernard Spencer, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• A nonlinear estimator for reconstructing the angular velocity of a spacecraft without rate gyros (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), by Michael E. Polites, W. D. Lightsey, and George C. Marshall Space Flight Center (page images at HathiTrust)
• Control of the meteoroid hazard to space vehicles (National Aeronautics and Space Administration, 1964), by Philip J. D'Anna, James J. Piechocki, Roger M. Heitz, Northrop Space Laboratories, 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)
• Motion effects on an IFR hovering task : analytical predictions and experimental results (National Aeronautics and Space Administration ;, 1971), by R. F. Ringland, Raymond E. Magdaleno, Robert L. Stapleford, Ames Research Center, and inc Systems Technology (page images at HathiTrust)
• Analytical method of approximating the motion of a spinning vehicle with variable mass and inertia properties acted upon by several disturbing parameters (U.S. G.P.O., 1961), by James J. Buglia (page images at HathiTrust)
• NASA TN D-2030 (National Aeronautics and Space Administration, 1963), by Paul G. Fournier, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TR R-362 (National Aeronautics and Space Administration ;, 1971), by Thomas W. Flatley, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TR R-187 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1964), by Helmut F. Bauer, George C. Marshall Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Secondary flow fields embedded in hypersonic shock layers (National Aeronautics and Space Administration :, 1962), by Alvin Seiff 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-5310 (National Aeronautics and Space Administration ;, 1969), by James H. Donohue, Harold P. Frisch, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5408 (National Aeronautics and Space Administration ;, 1969), by Delma C. Freeman, Richard D'Amato, Sue B. Grafton, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A passive method for scanning the celestial sphere (National Aeronautics and Space Administration ;, 1971), by A. J. Fleig and Goddard Space Flight Center (page images at HathiTrust)
• Effect of inertia properties on attitude stability of nonrigid spin-stabilized spacecraft (National Aeronautics and Space Administration ;, 1974), by W. E. Lang, J. P. Young, and Goddard Space Flight 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)
• Dynamic model investigation of touchdown stability of lunar-landing vehicles (National Aeronautics and Space Administration ;, 1967), by Robert W. Herr, H. Wayne Leonard, 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)
• Effects of certain control-system nonlinearities on stability and pointing of an attached double-gimbal experiment package in presence of random crew-motion disturbances (National Aeronautics and Space Administration ;, 1973), by J. D. Shaughnessy, Vilas D. Nene, Nelson J. Groom, and Langley Research Center (page images at HathiTrust)
• NASA TN D-1831 (National Aeronautics and Space Administration, 1963), by Helmut F. Bauer, George C. Marshall Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-3889 (National Aeronautics and Space Administration :, 1968), by Kenneth C. Weston, Manned Spacecraft Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Analytical and experimental investigation of forces and frequencies resulting from liquid sloshing in a spherical tank Andrew J. Stofan and Alfred L. Armstead. (National Aeronautics and Space Administration :, 1962), by Andrew J. Stofan, Alfred L. Armstead, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Measured steady-state performance of water vapor jets for use in space vehicle attitude control systems (National Aeronautics and Space Administration :, 1962), by Bruce E. Tinling and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5222 (National Aeronautics and Space Administration ;, 1969), by Richard M. Beam, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Wind-tunnel investigation at Mach numbers from 3.0 to 6.8 of the static aerodynamic characteristics of modified Mercury exit and escape capsule configurations (National Aeronautics and Space Administration, 1960), by Albin O. Pearson, Langley Research Center, and United States National Aeronautics and Space Administration (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)
• Low-subsonic-speed static longitudinal stability and control characteristics of a winged reentry-vehicle configuration having wingtip panels that fold up for high-drag reentry (National Aeronautics and Space Administration, 1960), by George M. Ware 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)
• 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)
• 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)
• 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)
• The USAF Stability and Control Digital Datcom. Volume III, Pilot module (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), by John E. Williams, Steven R. Vukelich, Air Force Flight Dynamics Laboratory (U.S.), McDonnell Douglas Astronautics Company-St. Louis, and United States. Air Force. Systems Command (page images at HathiTrust)
• Moment requirements and techniques (Wright-Patterson Air Force Base, Ohio : Flight Control Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), by Bendix Research Laboratories and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• The USAF Stability and Control Digital Datcom. Volume I, Users manual (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), by John E. Williams, Steven R. Vukelich, Air Force Flight Dynamics Laboratory (U.S.), McDonnell Douglas Astronautics Company-St. Louis, and United States. Air Force. Systems Command (page images at HathiTrust)
• The USAF Stability and Control Digital Datcom. Volume II, Implementtion of Datacom methods (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1976., 1976), by John E. Williams, Steven R. Vukelich, Air Force Flight Dynamics Laboratory (U.S.), McDonnell Douglas Astronautics Company-St. Louis, and United States. Air Force. Systems Command (page images at HathiTrust)
• The USAF Stability and Control Digital Datcom. Volume I, Users manual (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1976., 1976), by John E. Williams, Steven R. Vukelich, Air Force Flight Dynamics Laboratory (U.S.), McDonnell Douglas Astronautics Company-St. Louis, and United States. Air Force. Systems Command (page images at HathiTrust)

More items available under broader and related terms at left.