On the flight derived/aerodynamic data base performance comparisons for the NASA Space Shuttle entries during the hypersonic regime
- 10 January 1983
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Selected stability and control derivatives from the first three Space Shuttle entriesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Shuttle entry performance and stability and control derivatives extraction from flight measurement dataPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- A preliminary correlation of the orbiter stability and control aerodynamics from the first two Space Shuttle flights /STS-1 & 2/ with preflight predictionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Space Shuttle entry aerodynamic comparisons of flight 1 with preflight predictionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- An experiment for Shuttle aerodynamic force coefficient determination from inflight dynamical and atmospheric measurementsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978