High-Fidelity Thermal Protection System Sizing of Reusable Launch Vehicle
- 1 September 1997
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 34 (5) , 577-583
- https://doi.org/10.2514/2.3261
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Methodology for full-body TPS sizing of Access-to-Space vehiclesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1996
- Innovative economic development and technology integration for single stage to orbit (SSTO) conceptsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- Multiblock analysis for shuttle orbiter reentry heating from Mach 24 to Mach 12Journal of Spacecraft and Rockets, 1994
- High-resolution shock-capturing schemes for inviscid and viscous hypersonic flowsJournal of Computational Physics, 1990
- Comparison of finite volume flux vector splittings for the Euler equationsAIAA Journal, 1986