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: 250 s
Max Altitude: 60,000 feet
Cooling Method: ablative and film
What I do
FEA being conducted on MOE support plate
I conduct Finite Element Analysis and hand calculations on various MOE parts. This includes a engine mount plate to absorb the force of the engine during flight. I have also started FEA on the overall flight body, taking my experience from RED to now get Moe flying. ​
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In addition I help out with the hardware on our test stand. This ranges from basic work being done for test days such as loading up for a test day, pipe bending, or installing new flares and fitting, to more complicated tasks. Examples of some complicated work includes assembling the Moe engine and understanding how and where to put new valves on the feed system.
First Static Hotfire Attempt for Moe on 11/15/2025
