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Key Points and Specs
Purpose: Use for a vehicle to break collegiate world record for highest altitude liquid bi propellant engine
Propellant: Liquid Oxygen oxidizer and IPA based fuel.
Injector: Swirl
Burn Time: 15 seconds
Feed type: Pressure fed
Thrust: 2000 lbf
Height: 27 feet
ISP: 2752 s
Max Altitude: 60,000 feet
Cooling Method: ablative and film
What I do
I conduct Finite Element Analysis and hand calcs on various MOE parts. This includes a engine mount plate to absorb the force of the engine during flight and work on the COPV mount tanks to be used for holding the gas nitrogen feed system to propel Moe during flight.
Results from FEA on Moe engine plate
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