MR-106L 22N

Name: MR-106L 22N
Brand: Aerojet Rocketdyne

Vendor profile

Overview

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).

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Overview

Name: MR-106L 22N
Vendor: Aerojet Rocketdyne
Subsystem: Propulsion Subsystem
Component Type: Monopropellant Thruster
Form Factor: SmallSat
Heritage: Yes

Vendor Details

Name: Aerojet Rocketdyne
Website: https://www.rocket.com/
Founded: 1942

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Specifications

Subsystem: Propulsion Subsystem
Component Type: Monopropellant Thruster
Form Factor: SmallSat
Vendor: Aerojet Rocketdyne
Dry Mass: 0.59 kg
Average Power: 36.16 W
Heritage: Yes
Status: In Production

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