Simulated Air Launch Environment, Volume 2. Aeroheat Data Summary
Final rept. Sep 1972-May 1974
MORTON THIOKOL INC HUNTSVILLE AL HUNTSVILLE DIV
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A program was conducted in which the response and failure charactersitcs of solid propellant rocket motors when subjected to transient thermal conditions representing air launch operational environments were recorded and analyzed. Future Air Force mission profiles were used. The Maverick motor, AGM-65A, was used as a test bed on the program.
- Fluid Mechanics
- Solid Propellant Rocket Engines