John Beasley 1/31/2008 Propulsion Group: Solid and Hybrid Profiles AAE 450 Spring 2008
Solid: Burn Area Profiles AAE 450 Spring 2008 Propulsion Group
Hybrid: Burn and Port Area Profiles Cross Section AAE 450 Spring 2008 Propulsion Group
Assume constant ox flow rate Iterative process since fuel flow rate and burning rate are functions of each other Chamber pressure calculation also iterative since chamber pressure and characteristic velocity also interrelated Approach as taught in 539 AAE 450 Spring 2008
AAE 450 Spring 2008
AAE 450 Spring 2008