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Development of a reusable flightweight cryogenic storage systemA goldized-Kapton Superfloc multilayer insulation (MLI) coupled with an MLI purge and repressurization subsystem has been developed for use on reusable space vehicles. The subsystems were installed on an 87-inch diameter oblate spheroid liquid hydrogen tank and subjected to repeated space shuttle flight simulations to determine the effect upon system performance.
Document ID
19740053292
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Walburn, A. B. (General Dynamics Corp. Convair Aerospace Div., San Diego, Calif., United States)
Date Acquired
August 7, 2013
Publication Date
July 1, 1974
Subject Category
Space Vehicles
Report/Patent Number
AIAA PAPER 74-726
Report Number: AIAA PAPER 74-726
Meeting Information
Meeting: Thermophysics and Heat Transfer Conference
Location: Boston, MA
Start Date: July 15, 1974
End Date: July 17, 1974
Sponsors: American Society of Mechanical Engineers, American Institute of Aeronautics and Astronautics
Accession Number
74A36042
Funding Number(s)
CONTRACT_GRANT: NAS8-27419
Distribution Limits
Public
Copyright
Other

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