Minimum Cost Design (MCD) Material Screening. Test Report No. 1 - Haveg 41
AIR FORCE ROCKET PROPULSION LAB EDWARDS AFB CA
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This is the first 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 Haveg 41, an ablative composed of phenolic resin and asbestos fibers.
- Combustion and Ignition
- Rocket Engines