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Published bySimona Horvat Modified over 6 years ago
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John Beasley 2/14/2008 Propulsion Group Contact: MAT Analysis and Hybrid Rocket Engine Profiles
AAE 450 Spring 2008
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MAT Analysis: Material Trends
AAE 450 Spring 2008
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Hybrid Profiles Code Approach Assumptions
Calculate burn area and port area vs. burn distance for given geometry Guess Find actual value using: Calculate Find actual value using lookup table and Constant ox flow rate No spatial effects on burning Constant temp in throat for ablation rate calculation Conical nozzle No transients AAE 450 Spring 2008 Propulsion Group
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AAE 450 Spring 2008
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AAE 450 Spring 2008 Propulsion Group
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