High-Temperature Mechanical Properties of Strain Isolation Pad for Thermal Protection System
Author:
Affiliation:
1. Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China
Funder
Key Laboratory of Fundamental Science for National Defense-Advanced Design Technology of Flight Vehicle
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A34093
Reference11 articles.
1. Aerodynamic Heating of a Hypersonic Projectile with Forward-Facing Ellipsoid Cavity at Nose
2. Fluid-thermal analysis of aerodynamic heating over spiked blunt body configurations
3. Aerothermal Postflight Analysis of the Sharp Edge Flight Experiment-II
4. Aeroelastic Stability of Thermal Protection System for Inflatable Aerodynamic Decelerator
5. Characterization of Complex Porous Structures for Reusable Thermal Protection Systems: Porosity Measurements
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