MRM-122 130N

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Description

MRM-122 130N is a flight proven hydrazine monopropellant thruster. The thruster has a specific impulse of 217 to 228 sec and a thrust of 51 to 142 N (steady state).

 

Datasheet

Aerojet Rocketdyne – MRM-122 130N

Overview
NameMRM-122 130N
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
    Nominal Power43.0 W

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