MR-104J 440N
                        
                        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).
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Overview
- Name
 - MR-104J 440N
 - 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
 - 6.44 kg
 - Average Power
 - 88.0 W
 - Heritage
 - Yes
 - Status
 - In Production
 
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Aerojet Rocketdyne
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