Effect of ablation on the dynamics of spinning re-entry vehicles.
- 1 September 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 6 (9) , 1038-1044
- https://doi.org/10.2514/3.29752
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Effect of boundary-layer transition on vehicle dynamicsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969
- Effect of nose bluntness on the hypersonic unsteady aerodynamics of an ablating re-entry body.Journal of Spacecraft and Rockets, 1967
- Ablation effects on vehicle dynamics.Journal of Spacecraft and Rockets, 1966
- Influence of ablation on the dynamics of slender re-entry configurationsJournal of Spacecraft and Rockets, 1965
- FREE FLIGHT MOTION OF SYMMETRIC MISSILESPublished by Defense Technical Information Center (DTIC) ,1963