Plasmasphere from the DE 1 Retarding Ion Mass Spectrometer
Cassini Encounter with Earth: Planetary Magnetic Field Measurements
Lunar Helium-3: Mining Concepts, Extraction Research, and Potential ISRU Synergies
Lunar Helium-3: Mining Concepts, Extraction Research, and Potential ISRU Synergies
Development of the Dynamx Flight Instrument Prototype
Electrical Pressurization Concept for the Orion MPCV European Service Module Propulsion System
A low temperature facility for experiments on the International Space Station
The reconfiguration of the low temperature microgravity physics facility
Cryogenic And Thermal Aspects of The SIRTF Warm Launch Concept,
Microgravity Scaling Theory Experiment - Experiment Implementation Plan
Gas Contamination Effects on Pulse Tube Performance
LabVIEW Data Acquisition Onboard a NASA Micrograity Research Aircraft
A design study of a helium recovery system for mila. volume i- synopsis
Development of the Facet Cryostat
Development of the FACET Cryostat
The Lambda Point in a Low-g Simulator-Progress Report
High Resolution Thermometers for Ground and Space Utilization
The possibility of substituting helium for nitrogen in the cabins of spacecraft
Microwave Powered Airship System Design for High-Altitude Power Relay and Other Applications
A design study of a helium recovery system for mila, volume ii final report
Low Temperature Research in Microgravity
Lighter-Than-Air and Pressurized Structures Technology for Unmanned Aerial Vehicles (UAVs)
Analytical and experimental investigation of thermal and helium lift-pumping recirculation systems.
An Experimental Investigation of Stall Flutter of a Model Helicopter Rotor in Forward Flight
A large ultrahigh-vacuum environmental chamber with liquid-helium-cooled liner.
System Design for the Control of Liquid Helium by Electrostatic Forces for the Step Mission
Observations on man in an oxygen-helium environment at 380 mm. Hg total pressure. II - Respiratory.
Measurement of Magnetostriction Between 4.2 and 77K
Plasma Sterilization Technology for Spacecraft Applications
Evolvable Cryogenics (eCryo) Project Technology Workshop with Industry: Pressurization Test Results
Dynamic performance of Surveyor throttleable engine when propellants contain dissolved helium.