Subject: Space Shuttle Orbiter
Number of records: 75.
Iliff, Kenneth W. and Shafer, Mary F. (1993) A Comparison of Hypersonic Flight and Prediction Results. Meeting Paper AIAA-1993-0311, Research Engineering, NASA Dryden Flight Research Center.
Iliff, Kenneth W. and Shafer, Mary F. (1995) A Comparison of Hypersonic Vehicle Flight and Prediction Results. Technical Report NASA TM-104313, Research Engineering, NASA Dryden Flight Research Center.
Quinn, Robert D. and Gong, Leslie (2000) A Method for Calculating Transient Surface Temperatures and Surface Heating Rates for High-Speed Aircraft. Technical Report NASA/TP-2000-209034, Research Engineering, NASA Dryden Flight Research Center.
Anderson, Karl F. and Wrin, John W. and James, Robert (1986) A Radar Data Processing and Enhancement System. Technical Report NASA TM-88274, Research Engineering, NASA Dryden Flight Research Center.
Powers, Bruce G. (1984) Active Control Technology Experience With the Space Shuttle in the Landing Regime. Technical Report NASA TM-85910, Research Engineering, NASA Dryden Flight Research Center.
Saltzman, Edwin J. and Wang, K. Charles and Iliff, Kenneth W. (2002) Aerodynamic Assessment of Flight-Determined Subsonic Lift and Drag Characteristics of Seven Lifting-Body and Wing-Body Reentry Vehicle Configurations. Technical Report NASA/TP-2002-209032, Research Engineering, NASA Dryden Flight Research Center.
Iliff, Kenneth W. (1987) Aircraft Parameter Estimation- AIAA Dryden Lecture in Research for 1987. Technical Report NASA TM-88281, Research Engineering, NASA Dryden Flight Research Center.
Iliff, Kenneth W. (1987) Aircraft Parameter Estimation. Meeting Paper AIAA-1987-0623, Research Engineering, NASA Dryden Flight Research Center.
Haering Jr., Edward A. (1990) Airdata Calibration of a High-Performance Aircraft for Measuring Atmospheric Wind Profiles. Technical Report NASA TM-101714, Research Engineering, NASA Dryden Flight Research Center.
Bjarke, Lisa J. and Ehernberger, L. J. (1989) An In-Flight Technique for Wind Measurement in Support of the Space Shuttle Program. Technical Report NASA TM-4154, Research Engineering, NASA Dryden Flight Research Center.
Smith, John W. (1981) Analysis of a Longitudinal Pilot-Induced Oscillation Experienced on the Approach and Landing Test of the Space Shuttle. Technical Report NASA TM-81366, Research Engineering, NASA Dryden Flight Research Center.
Walker, Harold J. (1981) Analytic Study of Orbiter Landing Profiles. Technical Report NASA TM-81365, Research Engineering, NASA Dryden Flight Research Center.
Sarrafian, Shahan K. and Powers, Bruce G. (1985) Application of Frequency Domain Handling Qualities Criteria to the Longitudinal Landing Task. Meeting Paper AIAA-1985-1848, Research Engineering, NASA Dryden Flight Research Center.
Manke, John A. and Retelle, John P. and Kempel, Robert W. (1971) Assessment of Lifting Body Vehicle Handling Qualities. Meeting Paper AIAA-1971-310, Research Engineering, NASA Dryden Flight Research Center.
Carpenter, Richard (1970) Biotechnology Problems Relative to the Space Shuttle Vehicle, Meeting Paper AIAA-1970-1327, Research Engineering, NASA Flight Research Center.
Chiles, Harry R. (1983) Capture and Real-Time Display of Selected Space Shuttle Reentry Data.
Gong, Leslie and Ko, William L. and Quinn, Robert D. and Richards, W. Lance (1987) Comparison of Flight-Measured and Calculated Temperatures on the Space Shuttle Orbiter. Technical Report NASA TM-88278, Research Engineering, NASA Dryden Flight Research Center.
Privoznik, Cynthia M. and Berry, Donald T. (1986) Comparison of Pilot Effective Time Delay for Cockpit Controllers Used on Space Shuttle and Conventional Aircraft. Technical Report NASA TM-86030, Research Engineering, NASA Dryden Flight Research Center.
Carter, Alan L. and Sims, Robert L. (1981) Comparison of Theoretical Predictions of Orbiter Airloads with Wind Tunnel and Flight Test Results for a Mach Number of 0.52. Technical Report NASA TM-81358, Research Engineering, NASA Dryden Flight Research Center.
Day, Richard E. (1997) Coupling Dynamics in Aircraft: A Historical Perspective. NASA Special Publication SP-532, Research Engineering, NASA Dryden Flight Research Center. National Aeronautics and Space Administration.
Smith, John W. and Edwards, John W. (1980) Design of a Nonlinear Adaptive Filter for Suppression of Shuttle Pilot-Induced Oscillation Tendencies. Technical Report NASA TM-81349, Research Engineering, NASA Dryden Flight Research Center.
Trujillo, Bianca M. (1986) Determination of Lift and Drag Characteristics of Space Shuttle Orbiter Using Maximum Likelihood Estimation Technique. Meeting Paper AIAA-1986-2225, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Quinn, Robert D. and Gong, Leslie (1988) Effect of Internal Convection and Internal Radiation on the Structural Temperatures of Space Shuttle Orbiter. Technical Report NASA TM-100414, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Quinn, Robert D. and Gong, Leslie (1986) Effects of Forced and Free Convections on Structural Temperatures of Space Shuttle Orbiter During Reentry Flight. Technical Report NASA TM-86800 Revision, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Quinn, Robert D. and Gong, Leslie (1987) Effects of Forced and Free Convections on Structural Temperatures of Space Shuttle Orbiter During Reentry Flight. Meeting Paper AIAA-1987-1600, Research Engineering, NASA Dryden Flight Research Center.
Powers, Bruce G. (1980) Experience with an Adaptive Stick-Gain Algorithm to Reduce Pilot-Induced-Oscillation Tendencies. Meeting Paper AIAA-1980-1571, Research Engineering, NASA Dryden Flight Research Center.
Duke, Eugene L and Swann, Michael R. and Enevoldson, Einar K. and Wolf, Thomas D. (1983) Experience with Flight Test Trajectory Guidance. Journal of Guidance 6(5):393-398.
Swann, M.R. and Duke, E.L. and Enevoldson, E.K. and Wolf, T.D. (1981) Experience with Flight Test Trajectory Guidance. Meeting Paper AIAA-1981-2504, Research Engineering, NASA Dryden Flight Research Center.
Iliff, Kenneth W. and Shafer, Mary F. (1993) Extraction of Stability and Control Derivatives From Other Flight Data. Technical Report NASA TM-4500, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Quinn, Robert D. and Gong, Leslie (1986) Finite-Element Reentry Heat-Transfer Analysis of Space Shuttle Orbiter. Technical Report NASA TP-2657, Research Engineering, NASA Dryden Flight Research Center.
Fields, Roger A. (1992) Flight Vehicle Thermal Testing With Infrared Lamps. Technical Report NASA TM-4336, Research Engineering, NASA Dryden Flight Research Center.
Saltzman, Edwin J. and Wang, K. Charles and Iliff, Kenneth W. (1999) Flight-Determined Subsonic Lift and Drag Characteristics of Seven Lifting-Body and Wing-Body Reentry Vehicle Configurations With Truncated Bases. Meeting Paper AIAA-1999-0383, Research Engineering, NASA Dryden Flight Research Center.
Whitmore, Stephen A. (1985) Formulation and Implementation of Nonstationary Adaptive Estimation Algorithm With Applications to Air-Data Reconstruction. Technical Report NASA TM-86727, Research Engineering, NASA Dryden Flight Research Center.
Merlin, Peter W. (2006) Free Enterprise: Contributions of the Approach and Landing Test (ALT) Program to the Development of the Space Shuttle Orbiter. Conference Paper AIAA-2006-7467, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Gong, Leslie and Quinn, Robert D. (2004) Hypothetical Reentry Thermostructural Performance of Space Shuttle Orbiter With Missing or Eroded Thermal Protection Tiles. Technical Report NASA/TM-2004-212850, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. (1985) Impacts of Space Shuttle Thermal Protection System Tile on an F-15 Aircraft Vertical Tail. Technical Report NASA TM-85904, Research Engineering, NASA Dryden Flight Research Center.
Meyer Jr., Robert R. and Jarvis, Calvin R. and Barneburg, Jack (1981) In-Flight Aerodynamic Load Testing of the Shuttle Thermal Protection System. Meeting Paper AIAA-1981-2468, Research Engineering, NASA Dryden Flight Research Center.
Moes, Timothy R. and Meyer Jr., Robert R. (1990) In-Flight Investigation of Shuttle Tile Pressure Orifice Installations. Technical Report NASA TM-4219, Research Engineering, NASA Dryden Flight Research Center.
Trujillo, Bianca M. and Meyer Jr., Robert R. and Sawko, Paul M. (1983) In-Flight Load Testing of Advanced Shuttle Thermal Protection Systems. Technical Report NASA TM-86024, Research Engineering, NASA Dryden Flight Research Center.
Trujillo, Bianca M. and Meyer Jr., Robert R. and Sawko, Paul M. (1983) In-Flight Load Testing of Advanced Thermal Protection Systems. Meeting Paper AIAA-1983-2704, Research Engineering, NASA Dryden Flight Research Center.
Saltzman, Edwin J. and Wang, K. Charles and Iliff, Kenneth W. (2007) In-Flight Subsonic Lift and Drag Characteristics Unique to Blunt-Based Lifting Reentry Vehicles. Journal Article AIAA-18365, Research and Engineering, NASA Dryden Flight Research Center. Journal of Spacecraft and Rockets 44(2):299-309.
Maglieri, Domenic J. and Sothcott, Victor E. and Hicks, John (1990) Influence of Vehicle Configuration and Flight Profile on X-30 Sonic Booms. Meeting Paper AIAA-1990-5224 Research Engineering, NASA Dryden Flight Research Center.
Kock, Berwin M. and Fulton Jr, Fitzhugh L. and Drinkwater III, Fred J. (1972) Low-Lift-To-Drag-Ratio Approach and Landing Studies Using a CV-990 Airplane. Technical Report NASA Technical Note TN D-6732, Research Engineering, NASA Dryden Flight Research Center.
Banks, Daniel W. and Blanchard, Robert C. and Miller, Geoffrey M. (2004) Mobile Aerial Tracking and Imaging System (MATrIS) for Aeronautical Research. Technical Report NASA/TM-2004-212852, Research Engineering, NASA Dryden Flight Research Center.
Banks, D. W. and Blanchard, R. C. and Miller, G. M. (2004) Mobile Aerial Tracking and Imaging System (MATrIS) For Aeronautical Research. Meeting Paper ISFV106, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Olona, Timothy and Muramoto, Kyle M. (1990) Optimum Element Density Studies for Finite-Element Thermal Analysis of Hypersonic Aircraft Structures. Technical Report NASA TM-4163, Research Engineering, NASA Dryden Flight Research Center.
Smith, Mark S. (2006) Photogrammetric Trajectory Estimation of Foam Debris Ejected From an F-15 Aircraft. Technical Report NASA/TM-2006-213675, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Quinn, Robert D. and Gong, Leslie and Schuster, Lawrence S. and Gonzales, David (1981) Preflight Reentry Heat Transfer Analysis of Space Shuttle. Meeting Paper AIAA-1981-2382, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Schuster, Lawrence S. (1984) Preflight Transient Dynamic Analyses of B-52 Aircraft Carrying Space Shuttle Solid Rocket Booster Drop-Test Vehicle. Technical Report NASA TM-84925, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Schuster, Lawrence S. (1983) Preflight Transient Dynamic Analyses of B-52 Aircraft Carrying Space Shuttle Solid Rocket Booster Drop-Test Vehicle. Meeting Paper AIAA-1983-2698, Research Engineering, NASA Dryden Flight Research Center.
Authors, Various (1981) Preliminary Analysis of STS-1 Entry Flight Data. Technical Report NASA TM-81363, Research Engineering, NASA Dryden Flight Research Center.
Whitmore, Stephen A. (1983) Reconstruction of the Shuttle Reentry Air Data Parameters Using a Linearized Kalman Filter. Meeting Paper AIAA-1983-2097, Research Engineering, NASA Dryden Flight Research Center.
Iliff, Kenneth W. and Maine, Richard E. and Cooke, Douglas R. (1981) Selected Stability and Control Derivatives from the First Space Shuttle Entry. Meeting Paper AIAA-1981-2451, Research Engineering, NASA Dryden Flight Research Center.
Maine, Richard E. and Iliff, Kenneth W. (1982) Selected Stability and Control Derivatives from the First Three Space Shuttle Entries. Meeting Paper AIAA-1982-1318, Research Engineering, NASA Dryden Flight Research Center.
Cooper, Dale W. and James, Robert (1979) Shuttle Orbiter Radar Cross-Sectional Analysis. Technical Report NASA TM-72870, Research Engineering, NASA Dryden Flight Research Center.
Powers, Bruce G. and Sarrafian, Shahan K. (1986) Simulation Studies of Alternate Longitudinal Control Systems for the Space Shuttle Orbiter in the Landing Regime. Technical Report NASA TM-86815, Research Engineering, NASA Dryden Flight Research Center.
Powers, Bruce G. and Sarrafian, Shahan K. (1986) Simulation Studies of Alternate Longitudinal Control Systems for the Space Shuttle Orbiter in the Landing Regime. Meeting Paper AIAA-1986-2127, Research Engineering, NASA Dryden Flight Research Center.
Fisher, David F. (2007) Six Decades of Flight Research: An Annotated Bibliography of Technical Publications of NASA Dryden Flight Research Center, 1946-2006. Technical Report NASA/TP-2007-213684, Research and Engineering, NASA Dryden Flight Research Center.
Iliff, Kenneth W. and Shafer, Mary F. (1993) Space Shuttle Hypersonic Aerodynamic and Aerothermodynamic Flight Research and the Comparison to Ground Test Results. Technical Report NASA TM-4499, Research Engineering, NASA Dryden Flight Research Center.
Iliff, Kenneth W. and Shafer, Mary F. (1992) Space Shuttle Hypersonic Flight Research and the Comparison to Ground Test Results (Invited). Meeting Paper AIAA-1992-3988, Research Engineering, NASA Dryden Flight Research Center.
Andrews, William H. (1977) Space Shuttle Orbiter Approach and Landing Program Status. Meeting Paper AIAA-1977-1204, Research Engineering, NASA Dryden Flight Research Center.
Powers, Bruce G. (1984) Space Shuttle Pilot-Induced-Oscillation Research Testing.
Powers, Bruce G. (1984) Space Shuttle Pilot-Induced-Oscillation Research Testing. Technical Report NASA TM-86034, Research Engineering, NASA Dryden Flight Research Center.
Iliff, Kenneth W. and Maine, Richard E. and Cooke, Douglas R. (1983) Space Shuttle Stability and Control Derivatives Estimated from the First Entry. Journal of Guidance 6(4):264-271.
Carter, Alan L. (1982) Strain Gage Load Measurement on the Shuttle Orbiter. Technical Report NASA TM-84898, Research and Engineering, NASA Dryden Flight Research Center.
Nelson II, Sigurd A. (1994) Strain-Gage Selection in Loads Equations Using a Genetic Algorithm. Technical Report NASA CR-4597, Research Engineering, NASA Dryden Flight Research Center.
Larson, Terry J. and Siemers III, Paul M. (1981) Subsonic Tests of an All-Flush-Pressure-Orifice Air Data System. Technical Report NASA TP-1871, Research Engineering, NASA Dryden Flight Research Center.
Siemers III, Paul M. and Larson, Terry J. (1978) The Space Shuttle Orbiter and Aerodynamic Testing. Meeting Paper AIAA-1978-790, Research Engineering, NASA Dryden Flight Research Center.
Gong, Leslie and Ko, William L. and Quinn, Robert D. (1984) Thermal Response of Space Shuttle Wing During Reentry Heating. Technical Report NASA TM-85907, Research Engineering, NASA Dryden Flight Research Center.
Gong, Leslie and Ko, William L. and Quinn, Robert D. (1984) Thermal Response of Space Shuttle Wing During Reentry Heating. Meeting Paper AIAA-1984-1761, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Fields, Roger A. (1987) Thermal Stress Analysis of Space Shuttle Orbiter Subjected to Reentry Aerodynamic Heating. Technical Report NASA TM-88286, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Jenkins, Jerald M. (1987) Thermal Stress Analysis of Space Shuttle Orbiter Wing Skin Panel and Thermal Protection System. Technical Report NASA TM-88276, Research Engineering, NASA Dryden Flight Research Center.
Larson, Terry J. and Siemers III, Paul M. (1980) Use of Nose Cap and Fuselage Pressure Orifices for Determination of Air Data for Space Shuttle Orbiter Below Supersonic Speeds. Technical Report NASA TP-1643, Research Engineering, NASA Dryden Flight Research Center.
Beckner, Christine and Curry, Robert E. (1985) Water Tunnel Flow Visualization Using a Laser. Technical Report NASA TM-86743, Research Engineering, NASA Dryden Flight Research Center.
Larson, Terry J. and Flechner, Stuart G. and Siemers III, Paul M. (1980) Wind Tunnel Investigation of an All Flush Orifice Air Data System for a Large Subsonic Aircraft. Technical Report NASA TP-1642, Research Engineering, NASA Dryden Flight Research Center.
This list was generated on Sun Nov 22 18:17:06 PST 2009.
