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Research and Development in the Field of High Altitude Plastic Balloons
Structural Design for Aerodynamic Heating. Part II. Analytical Studies
The Variation of Heating Rates in a 1/30 Scale Booster Rocket Exhaust Jet
Air Launched Ballistic Radiosonde Dispenser Equipment
Application of Meteorological Rocket Systems
Atmospheric Entry of Manned Vehicles
In-Flight Structural Response of an HSS-1 Helicopter to a Nuclear Detonation
Environmental Control Study of Space Vehicles. Part III - Thermal Control Techniques and Systems
Structures for Space Operations
Effect of Firing Rocket Shells on the Performance of Turbojet Power Plant
Investigation of Battery Active Nickel Oxides Third Quarterly Report, 13 Dec. 1964 - 13 Mar. 1965
Beryllium Fabrication Methods Development Program - Thermal Treatment
An Analysis of a Charring Ablation Thermal Protection System
Large Astronomical Satellite Platform Arrangement
The Design and Manufacture of a 6 Inch Diameter Ablative Combustion Chamber
Structure and Materials Aspects of the Prime Flight Test Vehicle
Voyager Spacecraft. Volume V - Alternate Designs, Subsystems Considerations, Appendix I
Buckling and Steady Flutter of Heat-Compressed Panels in a Supersonic Flow
Reliability Analyses of Modular Power Conditioning and Control Systems for Ion Engines Final Report
156 Inch Fiberglass LITVC Motor Program. Volume 2
Solid Propellant Rocket Motor Performance Computer Programs Using the Group Transformation Method
Investigation of Stresses in the ALGOL II-B Rocket Nozzle Model Final Technical Report
The Initiation of Ignition in Composite Solid Rocket Propellants
Structural Design Concepts for Variable-Geometry Lifting Surfaces of Reentry Vehicles
Passive Temperature Control for Large Space Ships
Thermal Control Considerations for a Manned Orbiting Space Station