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Integrated hydrogen/oxygen technology applied to auxiliary propulsion systemsThe purpose of the Integrated Hydrogen/Oxygen Technology (IHOT) study was to determine if the vehicle/mission needs and technology of the 1990's support development of an all cryogenic H2/O2 system. In order to accomplish this, IHOT adopted the approach of designing Integrated Auxiliary Propulsion Systems (IAPS) for a representative manned vehicle; the advanced manned launch system. The primary objectives were to develop IAPS concepts which appeared to offer viable alternatives to state-of-the-art (i.e., hypergolic, or earth-storable) APS approaches. The IHOT study resulted in the definition of three APS concepts; two cryogenic IAPS, and a third concept utilizing hypergolic propellants.
Document ID
19910000803
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Gerhardt, David L.
(Rockwell International Corp. Downey, CA, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1990
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-185289
NAS 1.26:185289
Report Number: NASA-CR-185289
Report Number: NAS 1.26:185289
Accession Number
91N10116
Funding Number(s)
CONTRACT_GRANT: NAS3-25643
PROJECT: RTOP 506-42-31
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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