
Overview
MRM-122 130N is a flight proven hydrazine monopropellant thruster. The thruster has a specific impulse of 217 to 228 sec and a thrust of 51 to 142 N (steady state).
Properties
Overview
- Name
- MRM-122 130N
- Supplier
- L3Harris Aerojet Rocketdyne
- Type
- Other
- Flight proven
- Yes