The possibility of substituting helium for nitrogen in the cabins of spacecraft
A design study of a helium recovery system for mila. volume i- synopsis
A large ultrahigh-vacuum environmental chamber with liquid-helium-cooled liner.
A large ultrahigh-vacuum environmental chamber with liquid-helium-cooled liner.
Low Temperature Research in Microgravity
Cryogenic And Thermal Aspects of The SIRTF Warm Launch Concept,
The Lambda Point in a Low-g Simulator-Progress Report
High Resolution Thermometers for Ground and Space Utilization
System Design for the Control of Liquid Helium by Electrostatic Forces for the Step Mission
Gas Contamination Effects on Pulse Tube Performance
Measurement of Magnetostriction Between 4.2 and 77K