Experimental Dynamic Stability Characteristicsof a Shuttle Orbiter at M. = 8
- 1 July 1976
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 13 (7) , 424-429
- https://doi.org/10.2514/3.57103
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Effect of Sting Oscillations on the Measurement of Dynamic Stability DerivativesJournal of Aircraft, 1976