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Atomic hydrogen propellants: Historical perspectives and future possibilitiesAtomic hydrogen, a very high density free-radical propellant, is anticipated to generate a specific impulse of 600-1500 lb-f sec/lb-mass performance; this may facilitate the development of unique launch vehicles. A development status evaluation is presently given for atomic hydrogen investigations. It is noted that breakthroughs are required in the production, storage, and transfer of atomic hydrogen, before this fuel can become a viable rocket propellant.
Document ID
19930011425
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Palaszewski, Bryan
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1993
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-TM-106053
NAS 1.15:106053
E-7646
Meeting Information
Meeting: Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 11, 1993
End Date: January 14, 1993
Sponsors: AIAA
Accession Number
93N20614
Funding Number(s)
PROJECT: RTOP 506-42-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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