This paper discusses the current technologies for on-orbit refueling of spacecraft. The findings of 55 references are reviewed and summarized. Highlights include: (1) the Russian Progress system used by the International Space Station; (2) a flight demonstration of superfluid helium transfer; and (3) ground tests of large cryogenic systems. Key technologies discussed include vapor free liquid outflow, control of fluid inflow to prevent liquid venting, and quick disconnects for on-orbit mating of transfer lines.
Technologies for Refueling Spacecraft On-Orbit
Space 2000 ; 2000 ; Long Beach, CA, United States
2000-11-01
Preprint
Keine Angabe
Englisch
Technologies for refueling spacecraft on-orbit
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