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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).

Properties

Overview

Name
MRM-106F 40N
Supplier
L3Harris Aerojet Rocketdyne
Type
Other
Flight proven
Yes

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