Influence of ablation on the dynamics of slender re-entry configurations

Publisher Website

1 January 1965

journal article
Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets

Vol. 2 (1), 106-108
https://doi.org/10.2514/3.28133

Abstract

No abstract available

Keywords

This publication has 1 reference indexed in Scilit:

EFFECTS OF MASS ADDITION ON THE STABILITY OF SLENDER CONES AT HYPERSONIC SPEEDS
AIAA Journal, 1963

Cited by 15 articles