
Overview
MR-111G 4N is a flight proven hydrazine monopropellant thruster. The thruster has a total mass of 0.37 kg (includes engine, valves, and heaters), with a specific impulse of 219 to 229 sec and a thrust of 1.8 to 4.9 N (steady state).
Properties
Overview
- Name
- MR-111G 4N
- Supplier
- L3Harris Aerojet Rocketdyne
- Type
- Other
- Flight proven
- Yes