MR-104H 510N
Overview
MR-104H 510N is a flight proven hydrazine monopropellant thruster. The thruster has a total mass of 2.40 kg (includes engine and valves), with a specific impulse of 223 to 237 sec and a thrust of 201.0 to 554.2 N (steady state).
Overview
- Name
- MR-104H 510N
- 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
- 2.4 kg
- Average Power
- 60.1 W
- Heritage
- Yes
- Status
- In Production
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Aerojet Rocketdyne
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