Leak Detection Technique Improvement Study for Space Vehicles Final Report
Lightweight Pressurization System for the APOLLO Service Propulsion System Final Report
Basic Research on Liquid-Drop-Impact Erosion Quarterly Report, 8 Dec. 1966 - 8 Mar. 1967
Flight Control Systems and Launching Techniques for Air Ballast Systems
Description of the 120-Inch Hypersonic Shock Tunnel and Anticipated Performance
F M Telemetry and Free-Flight Techniques for Aerodynamic Measurements in Conventional Wind Tunnels
A design study of a helium recovery system for mila. volume i- synopsis
A design study of a helium recovery system for mila, volume ii final report
Analytical and experimental investigation of thermal and helium lift-pumping recirculation systems.
A large ultrahigh-vacuum environmental chamber with liquid-helium-cooled liner.
Effectiveness of Various Agents for Suppressing Ignition of RP-1 and Hydrogen under Flow Conditions
Pressurization System for Use in the APOLLO Service Propulsion System Interim Report
Pneumatic Control Rack Assemblies. Part No. 1541590 and 1503255. Operation and Service Manual
An Experimental Investigation of Stall Flutter of a Model Helicopter Rotor in Forward Flight
Evaluation Test of High Pressure Relief Valves 3200 and 6500 Psig
Captive Testing of Missile 14A at Mstsan-1, Edwards Air Force Base, Edwards, California