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Overview
MR-104H 510N is a flight proven hydrazine monopropellant thruster. The thruster has a total mass of 2.40 kg (includes engine and valves), with a specific impulse of 223 to 237 sec and a thrust of 201.0 to 554.2 N (steady state).
Properties
Overview
- Name
- MR-104H 510N
- Supplier
- L3Harris Aerojet Rocketdyne
- Type
- Other
- Flight proven
- Yes