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- The 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.
- Other Subject(s):
- NASA Technical Reports Server (NTRS) Collection.
- Document ID: 19730011155.
Accession ID: 73N19882.
- No Copyright.
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