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Abkühlen
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Transpiration and Film Cooling of Liquid Rocket Nozzles
Investigation of cooling problems at high chamber pressures final report, 1 jul. 1963 - 31 mar. 1965
[Research on a Self-Temperature Regulating Spacecraft Skin System]
Program for sea level test firing of rocket engines final report, 1 sep. 1964 - 1 feb. 1965
Design and testing of an aerospace dew point hygrometer Final report
Spacecraft temperature control by thermostatic fins Progress report, 1 Jun. - 30 Nov. 1965
Experimental investigation of two-stage air-cooled turbine suitable for flight at Mach 2.5
Summary of observed results when chilling the M-1 fuel turbopump to liquid hydrogen temperature
Spacecraft engine thrust chamber cooling final report, 13 may 1963 - 12 apr. 1964
Localized overheating in Aerobee regeneratively cooled thrust chambers