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Overview

MR-103J 1N is a flight proven hydrazine monopropellant thruster and is the predecessor to the MR-103G. The thruster has a total mass of 0.37 kg, with a specific impulse of 202 to 224 sec and a thrust of 0.19 to 1.13 N (steady state).

Properties

Overview

Name
MR-103J 1N
Supplier
L3Harris Aerojet Rocketdyne
Type
Other
Flight proven
Yes

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