MR-80B 3100N

Vendor profile
MR-80B 3100N image unavailable

Overview

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).

Specifications

Subsystem
Propulsion Subsystem
Component Type
Monopropellant Thruster
Form Factor
SmallSat
Vendor
Aerojet Rocketdyne
Dry Mass
168.0 kg
Average Power
23.75 W
Heritage
Yes
Status
In Production
Datasheet
  • Designer logo

    Try Designer

    Design, model, and evaluate satellite mission concepts quickly with our software.

    Launch designer

  • Aerojet Rocketdyne

    View all products

    • Similar Components

    MR-80B 3100N image unavailable

    MR-104H 510N

    Aerojet Rocketdyne

    MT-6

    IHI Aerospace

    MR-80B 3100N image unavailable

    CZ-11-600

    SITAEL

    MRM-106F 40N

    Aerojet Rocketdyne