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Technology issues associated with using densified hydrogen for space vehiclesSlush hydrogen and triple-point hydrogen offer the potential for reducing the size and weight of future space vehicles because these fluids have greater densities than normal-boiling-point liquid hydrogen. In addition, these fluids have greater heat capacities, which make them attractive fuels for such applications as the National Aerospace Plane and cryogenic depots. Some of the benefits of using slush hydrogen and triple-point hydrogen for space missions are quantified. Some of the major issues associated with using these densified cryogenic fuels for space applications are examined, and the technology efforts that have been made to address many of these issues are summarized.
Document ID
19920016034
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hardy, Terry L.
(NASA Lewis Research Center Cleveland, OH, United States)
Whalen, Margaret V.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1992
Subject Category
Propellants And Fuels
Report/Patent Number
NAS 1.15:105642
E-6988
AIAA PAPER 92-3079
NASA-TM-105642
Report Number: NAS 1.15:105642
Report Number: E-6988
Report Number: AIAA PAPER 92-3079
Report Number: NASA-TM-105642
Meeting Information
Meeting: Joint Propulsion Conference and Exhibit
Location: Nashville, TN
Country: United States
Start Date: July 6, 1992
End Date: July 8, 1992
Sponsors: ASEE, AIAA, ASME, SAE
Accession Number
92N25277
Funding Number(s)
PROJECT: RTOP 763-22-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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