Techniques for aerothermodynamic testing of ablating models in the wave superheater hypersonic tunnel
- 8 April 1968
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Influence of ablation on the dynamics of slender re-entry configurationsJournal of Spacecraft and Rockets, 1965