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Overview

MR-107U 300N is a flight proven hydrazine monopropellant thruster. The thruster has a total mass of 1.38 kg (includes engine and valves), with a specific impulse of 223 to 229 sec and a thrust of 182 to 307 N (steady state).

Properties

Overview

Name
MR-107U 300N
Supplier
L3Harris Aerojet Rocketdyne
Type
Other
Flight proven
Yes

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