Engineering Aerothermal Analysis for X-34 Thermal Protection System Design
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/2.3452
Reference38 articles.
1. The NASA Reusable Launch Vehicle Technology Program
2. Thermostructural Analysis of X-34 Wing Leading-Edge Tile Thermal Protection System
3. Thermal Protection Systems for Future Reusable Launch Vehicles
4. Heating Analysis of the Nosecap and Leading Edges of the X-34 Vehicle
5. Global Aeroheating Wind-Tunnel Measurements Using Improved Two-Color Phosphor Thermography Method
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