MR-106L 22N

Search
Generic filters
Description

MR-106L 22N is a flight proven hydrazine monopropellant thruster. The thruster has a total mass of 0.59 kg, with a specific impulse of 228 to 235 sec and a thrust of 10 to 34 N (steady state).

 

Datasheet

Aerojet Rocketdyne – MR-106L 22N

Overview
NameMR-106L 22N
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
    Mass0.59 kg
    Nominal Power36.16 W

    Resources