Development of Castable Carbonaceous Materials for Solid Rocket Nozzles
Final rept. Mar 1966-Mar 1969
MORTON THIOKOL INC BRIGHAM CITY UT WASATCH OPERATIONS
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Three basic material formulations were evaluated by laboratory testing and static firing in test motors with nozzles having a throat diameter of approximately 4 inches. In total, six nozzles were fabricated and static tested. One nozzle was fabricated of conventional nozzle materials and was used as a baseline. The remaining five nozzles were constructed using the castable carbonaceous materials.
- Laminates and Composite Materials
- Rocket Engines