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.
Arcjet Plasma Neutralization of Hall Thrusters I: Hybrid Thruster Mission Analysis
Cassini Encounter with Earth: Planetary Magnetic Field Measurements
Cryogenic And Thermal Aspects of The SIRTF Warm Launch Concept,
Dynamical Models for Sloshing Dynamics of Helium 2 Under Low-G Conditions
Effectiveness of Various Agents for Suppressing Ignition of RP-1 and Hydrogen under Flow Conditions