Minimum Cost Design (MCD) Material Screening. Test Report No. 4 - Plastonium 7.
AIR FORCE ROCKET PROPULSION LAB EDWARDS AFB CALIF
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This is the fourth of a series of reports describing the results of test firings conducted to determine the performance of low-cost ablative materials which are candidates for use as thrust chamber and nozzle liners for MCD Minimum Cost Design booster engines. This report describes the test of Plastonium 7, composed of phenolic microballoons and calcium sulfate crystals.
- Combustion and Ignition
- Rocket Engines