Europa 1 - Acceptance Testing of the Helium Charging System MK 2 for Third Stage Vehicle
Experimental Investigation of Containment in Constant-Temperature Radial-Inflow Vortexes
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