Electrical Pressurization Concept for the Orion MPCV European Service Module Propulsion System
A low temperature facility for experiments on the International Space Station
Development of the FACET Cryostat
Development of the Facet Cryostat
Development of the Dynamx Flight Instrument Prototype
Measurement of Magnetostriction Between 4.2 and 77K
Gas Contamination Effects on Pulse Tube Performance
LabVIEW Data Acquisition Onboard a NASA Micrograity Research Aircraft
Cryogenic And Thermal Aspects of The SIRTF Warm Launch Concept,
High Resolution Thermometers for Ground and Space Utilization
System Design for the Control of Liquid Helium by Electrostatic Forces for the Step Mission
Dynamic performance of Surveyor throttleable engine when propellants contain dissolved helium.
A design study of a helium recovery system for mila. volume i- synopsis
A design study of a helium recovery system for mila, volume ii final report
Analytical and experimental investigation of thermal and helium lift-pumping recirculation systems.
A large ultrahigh-vacuum environmental chamber with liquid-helium-cooled liner.