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Kühlsystem
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Aerospace America Year in Review -Thermophysics
The Edison Infrared Space Observatory and the Study of Extra-Solar Planetary Meterial
On the Nature of Io's Thermal Reservoir Unit
The Development of an Airborne Information Management System for Flight Test
Gaseous-film cooling of a rocket motor with injection near the throat
A probe for total-enthalpy measurements in arcjet exhausts.
Analytical solution of the ''known-heat-load'' space radiator problem.
Transpiration and Film Cooling of Liquid Rocket Nozzles
[Research on a Self-Temperature Regulating Spacecraft Skin System]
Summary of observed results when chilling the M-1 fuel turbopump to liquid hydrogen temperature
Localized overheating in Aerobee regeneratively cooled thrust chambers
Investigation of cooling problems at high chamber pressures final report, 1 jul. 1963 - 31 mar. 1965
A large ultrahigh-vacuum environmental chamber with liquid-helium-cooled liner.