Ballistic range tests of ablating and nonablating slender cones
- 1 March 1970
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 8 (3) , 558-564
- https://doi.org/10.2514/3.5705
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
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- Ablation testing in ballistic rangesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1968
- Dynamic stability wind-tunnel tests of a 10 deg cone with simulated ablation at m equals 17.AIAA Journal, 1967
- Boundary-layer transition on ablating cones at speeds up to 7 km/sec.AIAA Journal, 1966
- Ablation effects on vehicle dynamicsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1966
- Influence of ablation on the dynamics of slender re-entry configurationsJournal of Spacecraft and Rockets, 1965
- Effect of mass injection on the drag of a slender cone in hypersonic flowAIAA Journal, 1964
- EFFECTS OF MASS ADDITION ON THE STABILITY OF SLENDER CONES AT HYPERSONIC SPEEDSAIAA Journal, 1963
- A New Method for Computing Drag Coefficients from Ballistic Range DataJournal of the Aerospace Sciences, 1958
- ON THE FREE FLIGHT MOTION OF MISSILES HAVING SLIGHT CONFIGURATIONAL ASYMMETRIESPublished by Defense Technical Information Center (DTIC) ,1953