R-42DM 890N

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Description

The R-42DM 890N is a Biprop Thruster developed by Aerojet Rocketdyne. R-42DM 890N Biprop Thruster is designed for SmallSat with a mass of 7.3 kg and an average power consumption of 45 W.

 

Datasheet

Aerojet Rocketdyne – R-42DM 890N

Overview
NameR-42DM 890N
ManufacturerAerojet Rocketdyne
SubsystemPropulsion
ClassificationBiprop Thruster
Form FactorSmallSat
TRL9
HeritageYes
Vendor Overview
Vendor NameAerojet Rocketdyne
Vendor Websitehttps://www.rocket.com
Vendor LocationUnited States
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SPECIFICATIONS
SubsystemPropulsion
ClassificationBiprop Thruster
Form FactorSmallSat
VendorAerojet Rocketdyne
HeritageYes
Mass7.3 kg
Nominal Power45.0 W

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