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Key Points and Specs
Purpose: Demonstration of ability to make and test regen bi propellant engine, serve as basis for more complex engine designs.
Propellant: Liquid Oxygen and JetA
Injector: Swirl
Burn Time: 20 seconds
Feed type: Pressure fed
Thrust: 750 lbf
Number of Channels: 80
ISP: 231* s
What I Do
I work on leading several aspects of the design around RED, especially in regards to it's wider integration and flow systems to be used. In the future, I will oversee Red's production and test campaign.
RED has undergone a preliminary design review and is set for a critical review in January of 2026.
RED Liner
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