A space shuttle booster/orbiter atmospheric ascent guidance algorithm is developed that will reduce the aerodynamically induced structural loads as compared to an open loop guidance algorithm.
Structural load reduction of the space shuttle booster/orbiter configuration using a load relief guidance technique
1973-04-05
Report
Keine Angabe
Englisch
Space Shuttle Orbiter configuration case history
AIAA | 1978
|Space Shuttle Orbiter Guidance and Control System Design
SAE Technical Papers | 1974
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