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Space shuttle thermal scale modeling application studyThe critical thermal control problems and verification of thermal mathematical model results for the space shuttle concept are discussed. The use of a small scale thermal model of the space shuttle is proposed. It was determined that a one-third scale model of the space shuttle would serve as a useful tool throughout the entire thermal design and verification program. The major considerations in modeling the conduction-radiation-convection fields, the level of detail for modeling various systems, preliminary test requirements, and potential applications of the thermal scale model are summarized.
Document ID
19730011155
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Marshall, K. N.
(Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Foster, W. G.
(Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1973
Subject Category
Space Vehicles
Report/Patent Number
NASA-CR-128849
LMSC-D313907
TP-3613
Report Number: NASA-CR-128849
Report Number: LMSC-D313907
Report Number: TP-3613
Accession Number
73N19882
Funding Number(s)
CONTRACT_GRANT: NAS9-12991
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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