MR-111G 4N

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Description

MR-111G 4N is a flight proven hydrazine monopropellant thruster. The thruster has a total mass of 0.37 kg (includes engine, valves, and heaters), with a specific impulse of 219 to 229 sec and a thrust of 1.8 to 4.9 N (steady state).

 

Datasheet

Aerojet Rocketdyne – MR-111G 4N

Overview
NameMR-111G 4N
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
Mass0.37 kg
Nominal Power16.11 W

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