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.
System integration considerations for the Space Shuttle.
Short Course on the Space Shuttle Program ; 1972 ; Boulder, CO
1973-01-01
Miscellaneous
No indication
English
The Space Shuttle - Key considerations
NTRS | 1974
|Space shuttle structural fatigue considerations
NTRS | 1970
|Space shuttle ascent phase abort considerations
NTRS | 1970
|Space Shuttle Cargo Integration Assessments
British Library Conference Proceedings | 2002
|