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Overview

MR-111G 4N is a flight proven hydrazine monopropellant thruster. The thruster has a total mass of 0.37 kg (includes engine, valves, and heaters), with a specific impulse of 219 to 229 sec and a thrust of 1.8 to 4.9 N (steady state).

Properties

Overview

Name
MR-111G 4N
Supplier
L3Harris Aerojet Rocketdyne
Type
Other
Flight proven
Yes

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