
Overview
MR-103J 1N is a flight proven hydrazine monopropellant thruster and is the predecessor to the MR-103G. The thruster has a total mass of 0.37 kg, with a specific impulse of 202 to 224 sec and a thrust of 0.19 to 1.13 N (steady state).
Properties
Overview
- Name
- MR-103J 1N
- Supplier
- L3Harris Aerojet Rocketdyne
- Type
- Other
- Flight proven
- Yes