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
Advanced Liquid Oxygen (LO2) Propellant Conditioning Concept Testing
Aerospace Corporation Space Science Program Report to COSPAR, CY 72
A large ultrahigh-vacuum environmental chamber with liquid-helium-cooled liner.
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.
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