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design, fabrication, and application of insulation system to full-scale tankLightweight insulation system design, fabrication, installation, and weight breakdown for full scale Centaur tank
Document ID
19650010310
Document Type
Other
Authors
Burkley, R. A.
(GOODYEAR AEROSPACE CORP.)
Perkins, P. J., Jr.
(NASA Lewis Research Center Cleveland, OH, United States)
Shriver, C. B.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 2, 2013
Publication Date
March 1, 1965
Subject Category
THERMODYNAMICS AND COMBUSTION
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CENTAUR LAUNCH VEHICLE
THERMAL INSULATION
PROPELLANT TANK

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