A design study of a helium recovery system for mila, volume ii final report
A design study of a helium recovery system for mila. volume i- synopsis
ADR Configurations and Optimization for Cryocooler-Based Operation
Advanced Liquid Oxygen (LO2) Propellant Conditioning Concept Testing
A large ultrahigh-vacuum environmental chamber with liquid-helium-cooled liner.
A low temperature facility for experiments on the International Space Station
Analysis, Design and Performance of a 1.25 Inch Diameter Pneumatic Actuator
Analytical and experimental investigation of thermal and helium lift-pumping recirculation systems.
Analytical study of He II flow characteristics in the SHOOT transfer line
An assessment of helium gas behavior in SP-100 class reactors
An Experimental Investigation of Stall Flutter of a Model Helicopter Rotor in Forward Flight
An Investigation of Leakage of Large-Diameter O-Ring Seals on Spacecraft Air-Lock Hatches
APOLLO 9 Mission Report - Service Propulsion System Final Flight Evaluation, Supplement 5
Application of He-DCEN-TIG orbital welding to aluminium piping
A simplified sizing and mass model for axial flow turbines
Assessment of Lunar Sources of He-3 for Use on Earth
A superfluid pulse tube driven by a thermodynamically reversible magnetic pump
Basic Research on Liquid-Drop-Impact Erosion Quarterly Report, 8 Dec. 1966 - 8 Mar. 1967
Can He3 - He4 dilution refrigerators operate aboard spacecraft?
Captive Testing of Missile 14A at Mstsan-1, Edwards Air Force Base, Edwards, California
Coal gasification and other nuclear process heat applications
Cold Helium Gas Pressurization For Spacecraft Cryogenic Propulsion Systems
Colourless, nonradiant, blameless: a study of the hindenburg disaster
Correlation between gases and mass leak rate of gasketing materials
Cryocooler Working Medium Influence on Outgassing Rate
Cryogenic And Thermal Aspects of The SIRTF Warm Launch Concept,
Cryogenic whole air sampler system (Final rept. Sep 73 - May74)
Cryopumps for evacuating space simulation chambers
Current and Future Rocket Propulsion Testing at NASA Stennis Space Center
Cycles combines pour systemes nucleaires terrestres et spatiaux
DC discharge phenomena in artificial air for an undersea habitat