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Rechargeable metal hydrides for spacecraft applicationStoring hydrogen on board the Space Station presents both safety and logistics problems. Conventional storage using pressurized bottles requires large masses, pressures, and volumes to handle the hydrogen to be used in experiments in the U.S. Laboratory Module and residual hydrogen generated by the ECLSS. Rechargeable metal hydrides may be competitive with conventional storage techniques. The basic theory of hydride behavior is presented and the engineering properties of LaNi5 are discussed to gain a clear understanding of the potential of metal hydrides for handling spacecraft hydrogen resources. Applications to Space Station and the safety of metal hydrides are presented and compared to conventional hydride storage. This comparison indicates that metal hydrides may be safer and require lower pressures, less volume, and less mass to store an equivalent mass of hydrogen.
Document ID
19890000813
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Perry, J. L.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 5, 2013
Publication Date
September 1, 1988
Subject Category
Engineering (General)
Report/Patent Number
M-598
NAS 1.15:4076
NASA-TM-4076
Report Number: M-598
Report Number: NAS 1.15:4076
Report Number: NASA-TM-4076
Accession Number
89N10184
Funding Number(s)
PROJECT: RTOP 471-42
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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