MR-103J 1N
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).
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Overview
- Name
- MR-103J 1N
- 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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