John Beasley 2/14/2008 Propulsion Group Contact: MAT Analysis and Hybrid Rocket Engine Profiles AAE 450 Spring 2008
MAT Analysis: Material Trends AAE 450 Spring 2008
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
AAE 450 Spring 2008
AAE 450 Spring 2008 Propulsion Group