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Kühlsystem
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Structural Heat Intercept, Insulation and Vibration Evaluation Rig (SHIIVER)
Cyrogenic Life Support Technology Development Project
Launch Pad Closeout Operations for the Mars Science Laboratory's Heat Rejection System
Supercooling of thermoelectric device using a current pulse
A new architecture for avionics thermal management
Micro/nano spacecraft thermal control using MEMS-based pumped liquid cooling system
Mars Pathfinder mechanically pumped cooling loop
Solid-state power generation and cooling micro/nanodevices for distributed system architectures
MEMS based pumped liquid cooling systems for micro/nano spacecraft thermal control
Development of Flight Technology for Future Laser-Cooled Space Clocks
Development of Flight Technology for Future Laser-Cooled Space Clocks
Clock Technology Development for the Laser Cooling and Atomic Physics (LCAP) Program
Measurement of Magnetostriction Between 4.2 and 77K
Long Term Life Testing of a Mechanically Pumped Cooling Loop for Spacecraft Thermal Control
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.
Extraterrestrial cryogenic propellants reliquefaction.
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.
A radiation-cooled nuclear rocket nozzle for long firing durations.
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
Apollo portable life-support system - development status.
Devices for controlling thermal gradients in spacecraft structures