MR-103J 1N

Name: MR-103J 1N
Brand: Aerojet Rocketdyne

Vendor profile

Overview

MR-103J 1N is a flight proven hydrazine monopropellant thruster and is the predecessor to the MR-103G. The thruster has a total mass of 0.37 kg, with a specific impulse of 202 to 224 sec and a thrust of 0.19 to 1.13 N (steady state).

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Overview

Name: MR-103J 1N
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: 0.37 kg
Average Power: 16.11 W
Heritage: Yes
Status: In Production

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