NASA X Plane Document Collection DVD - X-15, X-1 & More

Description: The Historical Archive Sample Page NASA X Plane Document Collection on DVD Be sure to check out all our NASA Space History DVDS in our Store (Links open in a new window) This collection of 88 documents represents a comprehensive collection of 1000's of pages of material describing the the X plane missions in great detail. It includes everything from flight manuals to news releases to technical documents on the various spacecraft and instruments. Here are all the documents on this DVD. American X-Vehicles: An Inventory, X-1 to X-50 (NASA SP-2003-4531, Monograph 31). Aeronautics in Review - Aviation in Historical Perspective Quest for performance: The Evolution of Modern Aircraft NASA and General Aviation Airborne Trailblazer: Two decades with NASA Langley's 737 flying laboratory Compliation of papers summarizing some recent NASA research on manned military aircraft Configuration development study of the X-24C hypersonic research airplane Transonic Aerodynamic Characteristics of the Dyna-Soar Glider and Titan 3 Launch Vehicle Configuration with Various Fin Arrangements The History of the XV-15 Tilt Rotor Research Aircraft: From Concept to Flight PROGRESS IN AIRCRAFT DESIGN SINCE 1903 The Eclipse Project X-1 The hydrogen-peroxide rocket reaction-control system for the X-1B research airplane General handling-qualities results obtained during acceptance flight tests of the Bell XS-1 airplane Measurements of the wing and tail loads during the acceptance tests of bell XS-1 research airplane X-2 First landing of Bell X-2 research airplane X-3 High-speed landing loads measured on the Douglas X-3 research airplane X-4 Results obtained from second flight of X-4 airplane (A.F. no. 46-676) X-15 Hypersonics Before the Shuttle: A Concise History of the X-15 Research Airplane Alternate source The X-15 research aircraft- research accomplished and planned X-15 research results with a selected bibliography Component performance and flight operations of the X-15 research airplane program Thermal protection system X-15A-2 Design report Description of an energy management system for the X-15 Flight experience with shock impingement and interference heating on the X-15-2 research airplane Preliminary Results of Aerodynamic Heating Studies on the X-15 Airplane Heat-transfer measurements obtained on the X-15 airplane including correlations with wind-tunnel results GENERAL REVIEW OF PILOTING PROBLEMS ENCOUNTERED DURING SIMULATION AND FLIGHTS OF THE X-15 NINTH ANNUAL REPORT Research-Airplane-Committee report on Conference on the Progress of the X-15 project : a compilation of the papers presented, held at the IAS Building, Los Angeles, CA on 28-30 July 1958 Aerodynamic Characteristics of the X-15/B-52 Combination Review of the X-15 Program, June 1962 Piloting Performance During the Boost of the X-15 Airplane to High Altitude Experience with the X-15 adaptive flight control system Mission Planning and Operational Procedures for the X-15 Aircraft Structural Dynamics of the X-15 Aircraft Review of Technology Relating to the X-15 Project General Background of the X-15 Research-Airplane Project (1954) X-15 Analog and Digital Inertial Systems Flight Experience Summary of high-altitude and entry flight control experience with the X-15 airplane Summary of full-scale lift and drag characteristics of the X-15 airplane A study of display systems for manual guidance of large launch vehicles utilizing the X-15 airplane and flight simulators Technical note Research-Airplane-Committee Report on Conference on the progress of the X-15 project: a compilation of the papers presented, held at Langley Aeronautical Lab., Langley Field, VA on 25-26 October 1956 Operational experience with x-15 reaction controls Contributions of the x-15 program to lifting entry technology Measurements of loads, accelerations, and displacements of x-15 aircraft and landing gear during landing impact Aerodynamic forces on components of the X-15 airplane Resume of handling qualities of the X-15 airplane Pilot Considerations in the X-15 Research Airplane Program Research-Airplane-Committee report on Conference on the Progress of the X-15 Project Outline of the X-15 Project Landing gear behavior during touchdown of x-15 aircraft X-15 aircraft with interim engines during high altitude flying Flow-field investigations on the X-15 airplane and model up to hypersonic speeds YLR99-RM-1 rocket engine operating experience in the X-15 aircraft The X-15 Flight Control and Stability System Instrumentation for the X-15 Structural dynamics of the x-15 aircraft Analysis of X-15 Landing Approach and Flare Characteristics Determined from the First 30 Flights Hypersonic aerodynamic characteristics of two delta wing X-15 airplane configurations Operational experience with the x-15 reaction control and reaction augmentation systems Survey of operation and cost experience of the X-15 airplane as a reusable space vehicle Derived stability and control characteristics of x-15 aircraft from flight tests CONTROLLABILITY OF THE X-15 RESEARCH AIRPLANE WITH INTERIM ENGINES DURING HIGH-ALTITUDE FLIGHTS LANDING-GEAR BEHAVIOR DURING TOUCHDOWN AND RUNOUT FOR 17 LANDINGS OF THE X-15 RESEARCH AIRPLANE AERODYNAMIC AND CONTROL-SYSTEM CONTRIBUTIONS TO THE X-15 AIRPLANE LANDING-GEAR LOADS AERODYNAMICS-DERIVATIVE CHARACTERISTICS OF THE X-15 RESEARCH AIRPLANE AS DETERMINED FROM FLIGHT TESTS FOR MACH NUMBERS FROM 0.6 TO 3.4 ANALYTICAL INVESTIGATION AND PREDICTION OF SPIN AND RECOVERY CHARACTERISTICS OF THE NORTH AMERICAN X-15 AIRPLANE X-20 Dyna-Soar Transonic aerodynamic characteristics of the dyna-soar glider and Titan 3 launch vehicle configuration with various fin arrangements 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 Final report The wind-induced loads on a dynamically scaled model of the Dyna Soar glider and Titan 2 booster in launch position Longitudinal Aerodynamic Characteristics of Ten Booster-Glider Models for Project Dyna-Soar at Mach Numbers of 0.7 and 1.0 Joint Conference on Lifting Manned Hypervelocity and Reentry Vehicles. Part 2 A compilation of the papers presented Low-speed aerodynamic characteristics of a model of the DS-1 glider X-36 Flight Testing the X-36: The Test Pilots Perspective D-558 Scott Crossfield/Mach 2 Press Release Wind-tunnel investigation of the stability of jettisoned nose sections of the D-558 airplane : phases I and II Maximum altitude and maximum Mach number obtained with the modified Douglas D-558-II research airplane during demonstration flights Measured data pertaining to buffeting at supersonic speeds of the Douglas D-558-II research airplane LIFTING BODIES Wingless Flight: The Lifting Body Story Full scale wind tunnel investigation of the HL-10 manned lifting body flight vehicle Full-scale wind-tunnel investigation of the aerodynamic characteristics of the M2-F2 lifting body flight vehicle Stability and control characteristics of the M2-F2 lifting body measured during 16 glide flights Operational experiences and characteristics of the M2-F2 lifting body flight control system Developing and Flight Testing the HL-10 Lifting Body: A Precursor to the Space Shuttle Developing and flight testing the HL-10 lifting body: A precursor to the Space Shuttle Landing characteristics of a dynamic model of the HL-10 manned lifting entry vehicle Flight-determined stability and control characteristics of the M2-F3 lifting body vehicle Launch-pad abort capabilities of the HL-20 lifting body Lifting-Body Research Vehicles in a Low-Speed Flight Test Program Summary of an Advanced Manned Lifting Entry Vehicle Study Lift and drag characteristics of the M2-F2 lifting body during subsonic gliding flight Each document is presented in PDF format and is easily accessed from the menu contained on the DVD. 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End Time: 2024-04-30T18:13:25.000Z

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