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Spacecraft on-board propulsionThe topics presented are covered in viewgraph form and include the following: (1) planetary dual mode; and (2) space station H/O and H2O/gas resistojet. The major benefits identified by users are: (1) 280 kG payload for MMII CRAF class mission; and (2) eliminate orbiter/year and N2H4 COF.
Document ID
19930074439
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Byers, D. (NASA Headquarters Washington, DC United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1991
Publication Information
Publication: SSTAC(ARTS Review of the Draft Integrated Technology Plan (ITP). Volume 2: Propulsion Systems 8 p (SEE N93-71873 13-81)
Subject Category
Administration And Management
Report/Patent Number
PR13
Accession Number
93N71886
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19930074426Collected WorksSSTAC/ARTS Review of the Draft Integrated Technology Plan (ITP). Volume 2: Propulsion Systems
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