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Overview

MR-107S 275N is a flight proven hydrazine monopropellant thruster. The thruster has a total mass of 1.01 kg (includes engine, valves, and heaters), with a specific impulse of 225 to 236 sec and a thrust of 85 to 360. N (steady state).

Properties

Overview

Name
MR-107S 275N
Supplier
L3Harris Aerojet Rocketdyne
Type
Other
Flight proven
Yes

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