
Overview
MR-104J 440N is a flight proven hydrazine monopropellant thruster. There are two variants of the MR-104J, a 16.4 in and 20.5 in length. The thruster has a total mass of 6.44 kg (includes engine and valves), with a specific impulse of 215 to 223 sec and a thrust of 440 to 614 N (steady state).
Properties
Overview
- Name
- MR-104J 440N
- Supplier
- L3Harris Aerojet Rocketdyne
- Type
- Other
- Flight proven
- Yes