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Economic analysis of Perlite versus super insulation in liquid hydrogen storage and run vessels for the M-1 ProgramCost comparison of perlite and multilayer aluminum foil relective insulation in liquid hydrogen storage dewars for M-1 engine
Document ID
19660006079
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Commander, J. C. (Aerojet-General Corp. Covina, CA, United States)
Rotter, L. L. (Aerojet-General Corp. Covina, CA, United States)
Date Acquired
August 3, 2013
Publication Date
October 15, 1965
Subject Category
Facilities, Research, And Support
Report/Patent Number
AGC-8800-13
NASA-CR-54720
Report Number: AGC-8800-13
Report Number: NASA-CR-54720
Accession Number
66N15368
Funding Number(s)
CONTRACT_GRANT: NAS3-2555
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
THERMAL INSULATION
LIQUID HYDROGEN
DEWAR SYSTEM
M-1 ROCKET ENGINE
CRYOGENIC STORAGE

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