A REVIEW OF NOZZLE CONCEPTS FOR FUTURE SOLID PROPELLANT ROCKET MOTORS.
Special technical rept.,
PHILCO RESEARCH LABS NEWPORT BEACH CALIF
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This report is based on analyses and experiments performed under a contract entitled, Applied Research for Advanced Cooled Nozzles. A review is given of heat transfer and corrosion analyses, materials, and thermal protection methods for both cooled and uncooled rocket nozzles for present and future solid propellant rocket motors. Many of the details pertaining to this work can be found in report literature. Only the more pertinent aspects pertaining to rocket nozzles are presented. Author