Ablation testing in ballistic ranges

Publisher Website

8 April 1968

conference paper
Published by American Institute of Aeronautics and Astronautics (AIAA)

https://doi.org/10.2514/6.1968-385

Abstract

No abstract available

This publication has 2 references indexed in Scilit:

Dynamic stability wind-tunnel tests of a 10 deg cone with simulated ablation at m equals 17.
AIAA Journal, 1967
Effect of mass injection on the drag of a slender cone in hypersonic flow
AIAA Journal, 1964