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NASA X Plane
Document Collection on DVD

Price: $14.97     SKU: C667     Qty:

 

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. Here are the computer requirements to run and operate this DVD. You must have a PC running Windows or a Macintosh running OS X or higher software, a DVD drive and a web browser.

 

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Price: $14.97     SKU: C667     Qty:


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