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Kühlkreislauf
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The Edison Infrared Space Observatory and the Study of Extra-Solar Planetary Meterial
Transpiration and Film Cooling of Liquid Rocket Nozzles
AN EXPERIMENTAL INVESTIGATION OF GASEOUS-FILM COOLING OF A ROCKET MOTOR
Structural Heat Intercept, Insulation and Vibration Evaluation Rig (SHIIVER)
Aerospace America Year in Review -Thermophysics
Free-flight investigations of subliming ablators and transpiration cooling at hypersonic velocities
MEMS based pumped liquid cooling systems for micro/nano spacecraft thermal control
Experimental investigation of a lightweight rocket chamber
The effect of cooling-air blowers on thrust power
Supercooling of thermoelectric device using a current pulse
Ground-stand Cooling Investigation of an R-2600-22 Engine in a PBM-3D Nacelle
Clock Technology Development for the Laser Cooling and Atomic Physics (LCAP) Program
A new architecture for avionics thermal management
On the Nature of Io's Thermal Reservoir Unit
Effect of Exhaust Pressure on the Cooling Characteristics of an Air-cooled Engine
Gaseous-film cooling of a rocket motor with injection near the throat
Micro/nano spacecraft thermal control using MEMS-based pumped liquid cooling system
SELECTING A THRUST CHAMBER COOLING TECHNIQUE FOR SPACECRAFT ROCKET ENGINES
[Research on a Self-Temperature Regulating Spacecraft Skin System]
Development of Flight Technology for Future Laser-Cooled Space Clocks
Investigation of cooling problems at high chamber pressures final report, 1 jul. 1963 - 31 mar. 1965
A radiation-cooled nuclear rocket nozzle for long firing durations.
SELECTING A THRUST CHAMBER COOLING TECHNIQUE FOR SPACECRAFT ROCKET ENGINES
Ground-cooling and Flight Tests of an Airplane Equipped with a Nose-blower Engine Cowling
STUDY OF CHAMBER COOLING TECHNIQUES FOR SPACECRAFT ENGINES. MONTHLY LETTER
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
Summary of observed results when chilling the M-1 fuel turbopump to liquid hydrogen temperature
Altitude Performance Characteristics of Tail-pipe Burner with Variable-area Exhaust Nozzle
Development of Flight Technology for Future Laser-Cooled Space Clocks