MR-106L 22N
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Overview
MR-106L 22N is a flight proven hydrazine monopropellant thruster. The thruster has a total mass of 0.59 kg, with a specific impulse of 228 to 235 sec and a thrust of 10 to 34 N (steady state).
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Overview
- Name
- MR-106L 22N
- 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
- 0.59 kg
- Average Power
- 36.16 W
- Heritage
- Yes
- Status
- In Production
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Aerojet Rocketdyne
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