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Benefits of slush hydrogen for space missionsA study was performed to quantify the benefits of using slush hydrogen instead of normal boiling point liquid hydrogen as a fuel for several space missions. Vehicles considered in the study included the Space Shuttle/Shuttle-C, LEO to GEO transfer vehicles, Lunar and Mars transfer vehicles, and cryogenic depots in low Earth orbit. The advantages of using slush hydrogen were expressed in terms of initial mass differences at a constant payload, payload differences at a constant tank volume, and increases in fuel storage time for cryogenic depots. Both chemical oxygen/hydrogen and hydrogen nuclear thermal rocket propulsion were considered in the study. The results indicated that slush hydrogen offers the potential for significant decreases in initial mass and increases in payload for most missions studied. These advantages increase as the mission difficulty, or energy, increases.
Document ID
19920001996
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Friedlander, Alan
(Science Applications International Corp. Schaumburg, IL., United States)
Zubrin, Robert
(Martin Marietta Corp. Littleton, CO., United States)
Hardy, Terry L.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1991
Subject Category
Propellants And Fuels
Report/Patent Number
NASA-TM-104503
NAS 1.15:104503
E-6364
Accession Number
92N11214
Funding Number(s)
PROJECT: RTOP 763-01-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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