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Lunar excursion module -- Aerodynamics

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• Lunar excursion module
• Space vehicles -- Aerodynamics
• Aerodynamics

• Lunar excursion module -- Aerodynamics -- Testing

• 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)

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)

• 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)

• 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)

• 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)

• Experimental study of vertical impacts of an LM-type landing gear assembly under simulated lunar gravity (lunar module). (1968), by United States National Aeronautics and Space Administration, John Locke McCarty, Huey D. Carden, and Langley Research Center (page images at HathiTrust; US access only)
• 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)

• The High Resolution Accelerometer Package (HiRAP) flight experiment summary for the first 10 flights (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Robert C. Blanchard, K. T. Larman, M. Barrett, and Langley Research Center (page images at HathiTrust)
• Space shuttle orbiter trimmed center-of-gravity extension study : summary report (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by William I. Scallion, W. Pelham Phillips, and Langley Research Center (page images at HathiTrust)
• Analysis of the space shuttle orbiter entry dynamics from Mach 10 to Mach 2.5 with the November 1976 flight control system (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by Richard W. Powell, Howard W. Stone, and Langley Research Center (page images at HathiTrust)
• Influence of orbital-maneuvering-system fairings and rudder flare on the transonic aerodynamic characteristics of a space shuttle orbiter (National Aeronautics and Space Administration ;, 1975), by James C. Ellison and Langley Research Center (page images at HathiTrust)
• Analysis of separation of the space shuttle orbiter from a large transport airplane (National Aeronautics and Space Administration ;, 1977), by Alan W. Wilbite and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Influence of configuration details on the subsonic characteristics of a space shuttle orbiter design (National Aeronautics and Space Administration ;, 1974), by John P. Decker, W. Pelham Phillips, and Langley Research Center (page images at HathiTrust)
• Exploratory investigation of the aerodynamic characteristics of a biwing vehicle at Mach 20.3 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Peter T. Bernot and Langley Research Center (page images at HathiTrust)
• Experimental and predicted heating distributions for biconics at incidence in air at Mach 10 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by Charles G. Miller and Langley Research Center (page images at HathiTrust)
• NASA CR-1789 (National Aeronautics and Space Administration ;, 1972), by B. J. Kuchta, George R. Friedman, United States National Aeronautics and Space Administration, Langley Research Center, and General Dynamics Corporation. Convair Division (page images at HathiTrust)
• A study to determine the flight characteristics and handling qualities of variable geometry spacecraft. Volume III, Low L/D concept with fold-down wings (National Aeronautics and Space Administration ;, 1972), by George R. Friedman, B. J. Kuchta, Langley Research Center, and General Dynamics Corporation. Convair Division (page images at HathiTrust)
• On the dynamic characteristics of a variable-mass slender elastic body under high accelerations (National Aeronautics and Space Administration, 1967), by Leonard Meirovitch and Donald A. Wesley (page images at HathiTrust; US access only)
• High L/D concept with single pivot two position skewed wing (National Aeronautics and Space Administration ;, 1970), by B. J. Kuchta, Langley Research Center, and General Dynamics Corporation (page images at HathiTrust)
• Apollo experience report : flight anomaly resolution (National Aeronautics and Space Administration ;, 1975), by John D. Lobb and Lyndon B. Johnson Space Center (page images at HathiTrust)
• NASA TN D-3748 (National Aeronautics and Space Administration :, 1966), by William C. Moseley, Joseph C. Martino, Manned Spacecraft Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-4537 (National Aeronautics and Space Administration ;, 1968), by Alan D. Levin, Ronald C. Smith, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Viking entry vehicle aerodynamics at M = 2 in air and some preliminary test data for flight in CO₂ at M = 11 (National Aeronautics and Space Administration ;, 1975), by Robert I. Sammonds, Robert L. Kruse, and Ames Research Center (page images at HathiTrust)
• Subsonic and transonic dynamic stability characteristics of a space shuttle orbiter (National Aeronautics and Space Administration ;, 1975), by Richmond P. Boyden, Delma C. Freeman, and Langley Research Center (page images at HathiTrust)
• Supersonic dynamic stability characteristics of a space shuttle orbiter (National Aeronautics and Space Administration ;, 1976), by Delma C. Freeman, Edwin E. Davenport, Richmond P. Boyden, and Langley Research Center (page images at HathiTrust)
• NASA TN D-5859 (National Aeronautics and Space Administration :, 1970), by John M. Jerke, Atwood R. Heath, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Fixed-base visual simulation of pilot controlled descents of an advanced Apollo spacecraft with an all-flexible parawing (National Aeronautics and Space Administration ;, 1969), by G. Kimball Miller, Douglas B. Price, Byron M. Jacquet, and Langley Research Center (page images at HathiTrust)
• NASA TN D-5939 (National Aeronautics and Space Administration :, 1970), by Williard W. Anderson, Ralph W. Will, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-5897 (National Aeronautics and Space Administration :, 1970), by Robert S. Dunning, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5899 (National Aeronautics and Space Administration :, 1970), by Charles B. Johnson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-5565 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Marcus F. Heidmann, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-5339 (National Aeronautics and Space Administration ;, 1969), by Marcus F. Heidmann, John F. Groeneweg, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-5365 (National Aeronautics and Space Administration ;, 1969), by James F. Campbell, Josephine W. Grow, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Wind-tunnel investigation of the aerodynamic pressures on the Apollo command module configuration (National Aeronautics and Space Administration ;, 1969), by William C. Moseley, B. J. Wells, United States National Aeronautics and Space Administration, and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
• Entry aerodynamics at lunar return conditions obtained from the flight of Apollo 4 (AS-501) (National Aeronautics and Space Administration ;, 1969), by E. R. Hillje, United States National Aeronautics and Space Administration, and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
• A study of the aerodynamic characteristics of a fixed geometry paraglider configuration and three canopies with simulated variable canopy inflation at a mach number of 6.6 (National Aeronautics and Space Administration :, 1962), by Jim A. Penland and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Heat-transfer and pressure distributions for laminar separated flows downstream of rearward-facing steps with and without mass suction (National Aeronautics and Space Administration ;, 1974), by Ronald D. Brown, Antoni K. Jakubowski, and Langley Research Center (page images at HathiTrust)
• NASA TN D-5725 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by Willard W. Anderson, Kenneth L. Jacobs, Ralph W. Will, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Atomization, drop size, and penetration for cross-stream water injection at high-altitude reentry conditions with application to the RAM C-I and C-III flights (National Aeronautics and Space Administration ;, 1972), by Paul B. Gooderum, Dennis M. Bushnell, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• A real-gas study of low-density wedge-induced laminar separation on a highly cooled blunt flat plate at M [infinity]=12 (National Aeronautics and Space Administration, 1968), by John Benjamin Anders and C. L. W. Edwards (page images at HathiTrust)
• Experimental stability and control results at Mach 19 of an entry vehicle designed for an intermediate lift-drag ratio (National Aeronautics and Space Administration ;, 1968), by Patrick J. Johnston, Robert D. Witcofski, and Langley Research Center (page images at HathiTrust)
• Entry flight aerodynamics from Apollo Mission AS-202 (National Aeronautics and Space Administration ;, 1967), by E. R. Hillje and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
• Effectiveness of several control arrangements on a Mercury-type capsule (National Aeronautics and Space Administration, 1961), by Robert I. Sammonds, Robert R. Dickey, and Ames Research Center (page images at HathiTrust)
• Cape Canaveral wind and shear data (1 through 80 km) for use in vehicle design and performance studies (National Aeronautics and Space Administration, 1962), by James R. Scoggins, William W. Vaughan, George C. Marshall Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Wind-tunnel roll-damping measurements of a winged space shuttle configuration in launch attitude (National Aeronautics and Space Administration ;, 1973), by R. W. Hess, Edwin E. Davenport, and Langley Research Center (page images at HathiTrust)
• NASA TN D-6729 (National Aeronautics and Space Administration :, 1972), by Michael R. Galvas, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6697 (National Aeronautics and Space Administration :, 1972), by Ralph T. Dittrich, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Evaluation of flow properties behind 120-̊ and 140-̊included-angle cones and a Viking '75 entry vehicle at Mach numbers from 1.60 to 3.95 (National Aeronautics and Space Administration ;, 1973), by Clarence A. Brown, James F. Campbell, and Langley Research Center (page images at HathiTrust)
• A Method of accurately reducing the spin rate of a rotating spacecraft (National Aeronautics and Space Administration :, 1962), by Henry J. Cornille and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Wind flow in the 80-400 km altitude region of the atmosphere (National Aeronautics and Space Administration, 1963), by George C. Ragsdale, Peter E. Wasko, George C. Marshall Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Scientific satellites and the space environment (National Aeronautics and Space Administration, 1962), by John C. New, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-1966 (National Aeronautics and Space Administration, 1963), by E. Carson Yates, Annie G. Fox, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Chemical nonequilibrium effects on the inviscid flow in the windward plane of symmetry of two simplified shuttle configurations (National Aeronautics and Space Administration ;, 1973), by John A. Lordi, Charles B. Johnson, Robert J. Vidal, and Langley Research Center (page images at HathiTrust)
• NASA TN D-6583 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1971), by Ward F. Hodge, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Use of hexafluoroethane to simulate the inviscid real-gas effects on blunt entry vehicles (National Aeronautics and Space Administration ;, 1974), by James L. Hunt, Kathryn A. Smith, Robert A. Jones, and Langley Research Center (page images at HathiTrust)
• Wind-tunnel investigation at mach numbers from 0.30 to 1.14 of the static aerodynamic characteristics of modified Mercury escape and exit capsule configurations (National Aeronautics and Space Administration, 1961), by Albin O. Pearson 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)
• Wind-tunnel investigation of static aerodynamic characteristics of a 1/9-scale model of a Project Mercury capsule at mach numbers from 1.60 to 4.65 (National Aeronautics and Space Administration, 1960), by David S. Shaw, Kenneth L. Turner, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Wind-tunnel investigation at mach numbers from 0.50 to 1.14 of the static aerodynamic characteristics of a model of a Project Mercury capsule (National Aeronautics and Space Administration, 1960), by Albin O. Pearson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Ablation modeling for dynamic simulation of reentry vehicles : preprint (Wright Patterson Air Force Base, Ohio : Air Vehicles Directorte, Air Force Research Laboratory, Air Force Materiel Command, 2006., 2006), by David B. Doman, William B. Blake, and Ohio). Air Vehicles Directorate Air Force Research Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
• Stability derivatives of a 10° cone executing planar and nonplanar motion at Mach 14 (Wright-Patterson Air Force Base, Ohio : Aerospace Research Laboratories, Hypersonic Research Laboratory, Air Force Systems Commany, 1974., 1974), by Kevin E. Yelmgren, Otto Walchner, Frank M. Sawyer, Aerospace Research Laboratories (U.S.), and Hypersonic Research Laboratory (U.S.) (page images at HathiTrust)

More items available under broader and related terms at left.