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Overview

MRM-122 130N is a flight proven hydrazine monopropellant thruster. The thruster has a specific impulse of 217 to 228 sec and a thrust of 51 to 142 N (steady state).

Properties

Overview

Name
MRM-122 130N
Supplier
L3Harris Aerojet Rocketdyne
Type
Other
Flight proven
Yes

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