Engine

RED-1 will be the first liquid rocket engine with a turbopump tested by Texas A&M Rocket Engine Design. RED-1 is expected to be fully functional by May 2020.

Thrust: 2,500 lbs 

Fuel: Liquid Oxygen & Kerosene RP-1

Pressure: 1,300 psi

Mass Flow Rate: 5.567 slug per second

 

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