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Propellant transfer: Attached depotPropellant transfer at an attached depot involves: (1) resupply tankers (dedicated launch from the ground or scavenging from the external tank) to resupply the depot; (2) depot storage and supply tanks (attached, free-flyer, or tethered) from which liquid hydrogen and liquid oxygen are transferred to fill the space-based OTV; and (3) the space-based OTV which is resupplied with cryogens from the depot. Liquid storage and supply, thermal control, and transfer/resupply requirements for an attached depot are listed, and technologies defined. The specific fluid management elements and approaches for an attached depot are enumerated. The cryogenic fluid management facility (CFMF) shuttle attached-payload test bed, scheduled for a mid-1988 first launch, is expected to provide much of the needed technology.
Document ID
19850008696
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Eberhardt, R. N.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 12, 2013
Publication Date
April 1, 1984
Publication Information
Publication: NASA. Lewis Research Center OTV Propulsion Issues
Subject Category
Propellants And Fuels
Accession Number
85N17005
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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