MR-103G 1N

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Description

MR-103G 1N is a flight proven hydrazine monopropellant thruster. The thruster has a total mass of only 0.33 kg, with a specific impulse of 202 to 224 sec and a thrust of 0.19 to 1.13 N (steady state).

 

Datasheet

Aerojet Rocketdyne – MR-103G 1N

Overview
NameMR-103G 1N
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
Mass0.33 kg
Nominal Power16.11 W

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