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Kühlsystem
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MEMS based pumped liquid cooling systems for micro/nano spacecraft thermal control
Investigation of cooling problems at high chamber pressures final report, 1 jul. 1963 - 31 mar. 1965
Extraterrestrial cryogenic propellants reliquefaction.
SELECTING A THRUST CHAMBER COOLING TECHNIQUE FOR SPACECRAFT ROCKET ENGINES
A large ultrahigh-vacuum environmental chamber with liquid-helium-cooled liner.
AN EXPERIMENTAL INVESTIGATION OF GASEOUS-FILM COOLING OF A ROCKET MOTOR
Aerospace America Year in Review -Thermophysics
Transpiration and Film Cooling of Liquid Rocket Nozzles
The Edison Infrared Space Observatory and the Study of Extra-Solar Planetary Meterial
Free-flight investigations of subliming ablators and transpiration cooling at hypersonic velocities
Supercooling of thermoelectric device using a current pulse
Structural Heat Intercept, Insulation and Vibration Evaluation Rig (SHIIVER)
Experimental investigation of a lightweight rocket chamber
The effect of cooling-air blowers on thrust power
Gaseous-film cooling of a rocket motor with injection near the throat
Ground-stand Cooling Investigation of an R-2600-22 Engine in a PBM-3D Nacelle
A Method for the Design of Cooling Systems for Aircraft Power-plant Installations
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
Micro/nano spacecraft thermal control using MEMS-based pumped liquid cooling system
Effect of Exhaust Pressure on the Cooling Characteristics of an Air-cooled Engine
Engine Tests of Pressurized Shunt-type Cooling Systems for a Liquid-cooled Engine
Development of Flight Technology for Future Laser-Cooled Space Clocks
SELECTING A THRUST CHAMBER COOLING TECHNIQUE FOR SPACECRAFT ROCKET ENGINES
An analysis of supersonic aerodynamic heating with continuous fluid injection
[Research on a Self-Temperature Regulating Spacecraft Skin System]
A radiation-cooled nuclear rocket nozzle for long firing durations.
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