MR-104J 440N

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Description

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).

 

Datasheet

Aerojet Rocketdyne – MR-104J 440N

Overview
NameMR-104J 440N
ManufacturerAerojet Rocketdyne
SubsystemPropulsion
ClassificationMonoprop Thruster
Form FactorSmallSat
TRL9
HeritageYes
Vendor Overview
Vendor NameAerojet Rocketdyne
Vendor Websitehttps://www.rocket.com
Vendor LocationUnited States
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SPECIFICATIONS
SubsystemPropulsion
ClassificationMonoprop Thruster
Form FactorSmallSat
VendorAerojet Rocketdyne
HeritageYes
Mass6.44 kg
Nominal Power88.0 W

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