MR-111G 4N
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).
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Overview
- Name
- MR-111G 4N
- Vendor
- Aerojet Rocketdyne
- Subsystem
- Propulsion Subsystem
- Component Type
- Monopropellant Thruster
- Form Factor
- SmallSat
- Heritage
- Yes
Vendor Details
- Name
- Aerojet Rocketdyne
- Website
- https://www.rocket.com/
- Founded
- 1942
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Specifications
- Subsystem
- Propulsion Subsystem
- Component Type
- Monopropellant Thruster
- Form Factor
- SmallSat
- Vendor
- Aerojet Rocketdyne
- Dry Mass
- 0.37 kg
- Average Power
- 16.11 W
- Heritage
- Yes
- Status
- In Production
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Aerojet Rocketdyne
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