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NASA NTRS · 20150000198

Cryogenic Boil-Off Reduction System Testing

Abstract

The Cryogenic Boil-Off Reduction System was tested with LH2 and LOX in a vacuum chamber to simulate space vacuum and the temperatures of low Earth orbit. Testing was successful and results validated the scaling study model that predicts active cooling reduces upper stage cryogenic propulsion mass for loiter periods greater than 2 weeks.

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BibTeXRIS

Plachta, David W., Johnson, Wesley L., Feller, Jeffery. 2014-07-28. Cryogenic Boil-Off Reduction System Testing. https://ntrs.nasa.gov/citations/20150000198

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