Fundamental Modeling and Thermal Performance Issues for Metallic Thermal Protection System Concept
- 1 March 2004
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 41 (2) , 195-206
- https://doi.org/10.2514/1.9182
Abstract
No abstract availableKeywords
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- Preliminary Thermal-Mechanical Sizing of a Metallic Thermal Protection SystemJournal of Spacecraft and Rockets, 2004
- Metallic Thermal Protection System Requirements, Environments, and Integrated ConceptsJournal of Spacecraft and Rockets, 2004
- Application of experimental design methods to assess the effect of uncertain boundary conditions in inverse heat transfer problemsInternational Journal of Heat and Mass Transfer, 1998
- Approximate method for calculating heating rates on three-dimensional vehiclesJournal of Spacecraft and Rockets, 1994