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Overview
MR-107S 275N is a flight proven hydrazine monopropellant thruster. The thruster has a total mass of 1.01 kg (includes engine, valves, and heaters), with a specific impulse of 225 to 236 sec and a thrust of 85 to 360. N (steady state).
Properties
Overview
- Name
- MR-107S 275N
- Supplier
- L3Harris Aerojet Rocketdyne
- Type
- Other
- Flight proven
- Yes