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Kühlsystem
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Design and testing of an aerospace dew point hygrometer Final report
Spacecraft engine thrust chamber cooling final report, 13 may 1963 - 12 apr. 1964
Investigation of cooling problems at high chamber pressures final report, 1 jul. 1963 - 31 mar. 1965
Investigation of Cooling Problems at High Chamber Pressures Final Report, 1 Jul. 1963 - 31 Mar. 1965
Investigation of Cooling Problems at High Chamber Pressures Final Report, 1 Jul. 1963 - 31 Mar. 1965
Program for Sea Level Test Firing of Rocket Engines Final Report, 1 Sep. 1964 - 1 Feb. 1965
Spacecraft temperature control by thermostatic fins Progress report, 1 Jun. - 30 Nov. 1965
Spacecraft Temperature Control by Thermostatic Fins Progress Report, 1 Jun. - 30 Nov. 1965
Program for sea level test firing of rocket engines final report, 1 sep. 1964 - 1 feb. 1965
Vapor-Chamber Fin Studies Quarterly Report, May 28 - Aug. 28, 1965
Analytical Study of Moderator Wall Cooling of Gaseous Nuclear Rocket Engines
Vapor-Chamber Fin Studies First Quarterly Report, May 28 - Aug. 28, 1965
Subsurface Transportation Methods in Deep Snow
Effect of Power Dissipation on the Platform Temperatures of the L.A.S
Beryllium Fabrication Methods Development Program - Thermal Treatment
Preproduction Prototype Package Ventilation Kit, Second Structural and Human Factors Test
Engineering Design Handbook. Automotive Series. The Automotive Assembly
Air Force Rocket Propulsion Laboratory Scientific and Engineering Seminar Abstracts
Transpiration and Film Cooling of Liquid Rocket Nozzles
Transpiration and Film Cooling of Liquid Rocket Nozzles
Study of Novel Refrigeration Methods Final Report
Polar Camp Improvements Requirements and Concepts for Covered Storage Facilities
Feasibility Study of a Heat-Actuated Environmental Control System for the Navy F-4 Fighter Aircraft
Feasibility Study of a Heat-Actuated Environmental Control System for the Navy F-4 Fighter Aircraft
[Research on a Self-Temperature Regulating Spacecraft Skin System]
Programming a Digital Simulation Model of a Freeway Diamond Interchange
Localized Overheating in Aerobee Regeneratively Cooled Thrust Chambers
Vapor-Chamber Fin Studies Quarterly Report, Sep. 1 - Nov. 30, 1965
Summary of observed results when chilling the M-1 fuel turbopump to liquid hydrogen temperature
Localized overheating in Aerobee regeneratively cooled thrust chambers
Experimental Snow Plenum Air Cooling System for Byrd Station, Antarctica
United States Department of Commerce Auto-on-Train Project Equipment Review
Protective Structures and Components: Compilation of Abstracts