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Cryogenic fluid transfer - orbital transfer vehicleFluid transfer requirements are presented for the orbital transfer vehicle (OTV) issues such as OTV configuration, hardware design and size are taken into consideration. Tank chilldown, tank fill and thermodynamic properties are all evaluated in relationship to fluid transfer needs.
Document ID
19830002927
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hastings, L. J. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1982
Publication Information
Publication: NASA. Johnson Space Center Satellite Serv. Workshop, Vol. 1
Subject Category
Space Transportation
Accession Number
83N11197
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19830002905Collected WorksSatellite Services Workshop, Volume 1
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