MR-80B 3100N

Search
Generic filters
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
Vendor Request for Information Form

    Name *

    Email *

    Country *

    Would you like suggestions about similar products/services from other suppliers?

    Inquiry Description *

    SPECIFICATIONS
    SubsystemPropulsion
    ClassificationMonoprop Thruster
    Form FactorSmallSat
    VendorAerojet Rocketdyne
    HeritageYes
    Mass168.0 kg
    Nominal Power23.75 W

    Resources