R-40 3870N

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Description

The R-40 3870N is a Biprop Thruster developed by Aerojet Rocketdyne. R-40 3870N Biprop Thruster is designed for SmallSat with a mass of 10.5 kg and an average power consumption of 70 W.

 

Datasheet

Aerojet Rocketdyne – R-40 3870N

Overview
NameR-40 3870N
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
    Mass10.5 kg
    Nominal Power70.0 W

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