MR-401 0.09N

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Description

MR-501 0.09N is a flight proven hydrazine monopropellant thruster. The thruster has a total mass of 0.60 kg, with a specific impulse of 180 to 184 sec (steady state) and a thrust of 0.07 to 0.09 N (steady state).

 

Datasheet

Aerojet Rocketdyne – MR-401 0.09N

Overview
NameMR-401 0.09N
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
    Mass0.6 kg
    Nominal Power11.95 W

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