Thermostructural Analysis of X-34 Wing Leading-Edge Tile Thermal Protection System
- 1 March 1999
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 36 (2) , 189-198
- https://doi.org/10.2514/2.3449
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Heating Analysis of the Nosecap and Leading Edges of the X-34 VehicleJournal of Spacecraft and Rockets, 1999
- Ablation and thermal response program for spacecraft heatshield analysisPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1998
- Gas permeability of rigid fibrous refractory insulationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1997
- Solution strategy for thermal response of nonablating thermal protection systems at hypersonic speedsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1996