NASA NTRS · 19730052798
System integration considerations for the Space Shuttle.
Abstract
Description of some system integration studies which were carried out to define design requirements ensuring compatibility and satisfactory performance of individual Space Shuttle elements. Studies considered include definition of a vehicle concept providing a tradeoff between development and flight costs, evaluation of the need for booster thrust vector control, and analysis of optimum methods for vehicle control in aerodynamic flight.
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Silveira, M. A.. 1973-01-01. System integration considerations for the Space Shuttle.. https://ntrs.nasa.gov/citations/19730052798
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