MRM-106F 40N

MRM-106F 40N image

Overview

MRM-106F 40N is a flight proven hydrazine monopropellant thruster. The thruster has a total mass of 2.23 kg, with a specific impulse of 231 sec and a thrust of 40 N per rocket (steady state).

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Overview

Name
MRM-106F 40N
Form Factor
SmallSat
Heritage
Yes

Vendor Details

Name
Aerojet Rocketdyne
Founded
1942

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Specifications

Form Factor
SmallSat
Dry Mass
2.23 kg
Average Power
20.1 W
Heritage
Yes
Status
In Production
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