Minimum Cost Design (MCD) Material Screening, Test Report No. 5 - General Electric 223-50.
AIR FORCE ROCKET PROPULSION LAB EDWARDS AFB CALIF
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This is the fifth 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 General Electric 223-50, an ablative composed of epoxy novolac resin filled with silica powder and fibers.
- Combustion and Ignition
- Rocket Engines