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Optimization of base thermal protection system for advanced Saturn II boosters employing strap-on solid-propellant motors.Optimization of base thermal protection system for advanced Saturn II boosters employing strap-on solid propellant motors
Document ID
19670064186
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Adler, B. K.
Hammond, M. B.
Korkan, K. D.
Date Acquired
August 3, 2013
Publication Date
November 1, 1967
Subject Category
Thermodynamics And Combustion
Accession Number
67A42915
Funding Number(s)
CONTRACT_GRANT: NAS8-20265
Distribution Limits
Public
Copyright
Other
Keywords
SOLID PROPELLANT ROCKET ENGINE
THERMAL RADIATION
THERMAL PROTECTION
HEAT TRANSFER
SATURN LAUNCH VEHICLE
CERAMIC HONEYCOMB

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