MR-107S 275N

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Description

MR-107S 275N is a flight proven hydrazine monopropellant thruster. The thruster has a total mass of 1.01 kg (includes engine, valves, and heaters), with a specific impulse of 225 to 236 sec and a thrust of 85 to 360. N (steady state).

 

Datasheet

Aerojet Rocketdyne – MR-107S 275N

Overview
NameMR-107S 275N
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
Mass1.01 kg
Nominal Power52.0 W

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