MR-80B 3100N

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Description

MR-80B 3100N is a flight proven 22.12 inch long hydrazine monopropellant thruster. The thruster has a total mass of 168 kg (includes engine and valves), with a specific impulse of 200 to 225 sec and a thrust of 31 to 3603 N (steady state).

 

Datasheet

Aerojet Rocketdyne – MR-80B 3100N

Overview
NameMR-80B 3100N
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
Mass168.0 kg
Nominal Power23.75 W

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