High Viscosity Thermal Protection Materials.
Summary rept. 1 Jul 67-30 Jun 68,
NAVAL ORDNANCE LAB WHITE OAK MD
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Initial objectives of this work were to develop a high temperature resistant material capable of withstanding rocket nozzle throat, leading edge, or re-entry environments by virtue of its high temperature strength, resistance to oxidation, and ability to cool itself ablatively. Author
- Metallurgy and Metallography
- Rocket Engines