MRM-106F 40N

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Description

MRM-106F 40N is a flight proven hydrazine monopropellant thruster. The thruster has a total mass of 2.23 kg, with a specific impulse of 231 sec and a thrust of 40 N per rocket (steady state).

 

Datasheet

Aerojet Rocketdyne – MRM-106F 40N

Overview
NameMRM-106F 40N
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
Mass2.23 kg
Nominal Power20.1 W

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