
Overview
MRM-106F 40N is a flight proven hydrazine monopropellant thruster. The thruster has a total mass of 2.23 kg, with a specific impulse of 231 sec and a thrust of 40 N per rocket (steady state).
Properties
Overview
- Name
- MRM-106F 40N
- Supplier
- L3Harris Aerojet Rocketdyne
- Type
- Other
- Flight proven
- Yes