Thermomechanical Erosion of Ablative Plastic Composites.
Technical rept. May 69-Jun 71,
AVCO SYSTEMS DIV WILMINGTON MASS
Pagination or Media Count:
An analytical technique has been developed to predict the thermomechanical erosion of plastic composite materials for reentry nose tip application. The method presented requires empirically derived material property data which has been obtained for reverse chevron carbon phenolic from a series of 50 MW arc tests. The method has been used to predict the ablation behavior of similar materials in other test environments and is shown to be in reasonable agreement with the measured data. Author, modified-PL
- Laminates and Composite Materials
- Guided Missile Reentry Vehicles
- Unmanned Spacecraft