The development and application of aerodynamic uncertainties in the design of the entry trajectory and flight control system of the SpaceShuttle Orbiter

Author:

GAMBLE J.1,YOUNG J.1

Affiliation:

1. NASA, Johnson Space Center, Houston, TX

Publisher

American Institute of Aeronautics and Astronautics

Reference8 articles.

1. Young, James.; Underwood, Jimmy.; The Development of Aerodynamic Uncertainties for the Space Shuttle Orbiter, AlAA Paper 82-063.

2. Weil, Joseph; Powers, B. 8.: Correlation of Predicted and Flight Derived Stability Derivatives with Particular Application to Tailless Delta Wing Configurations, NASA TM-81361.

3. Kanipe, David 6.; PlumeIFlowfield Jet Interaction Effects on the Space Shuttle Orbiter During Entry: AIAA-82-11319,Aug. 9, 198;

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