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Liquid hydrogen/oxygen external tank development for the Space ShuttleThe evolution of the Space Shuttle System using an expendable External Tank was discussed. The reasoning for the cryogenic propellant selection for the Space Shuttle Main Engine was addressed. The unique problems, solutions, and design features imposed on the External Tank by the cryogenic propellants was discussed with special emphasis on the use of cryogenic insulation for aerodynamic heating protection. Manufacturing techniques for high production rate cryogenic tankage concluded the report.
Document ID
19790061571
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Odom, J. B. (NASA Marshall Space Flight Center Huntsville, Ala., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: Hydrogen for energy distribution; Symposium
Location: Chicago, IL
Start Date: July 24, 1978
End Date: July 28, 1978
Accession Number
79A45584
Distribution Limits
Public
Copyright
Other

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