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Overview

MR-104J 440N is a flight proven hydrazine monopropellant thruster. There are two variants of the MR-104J, a 16.4 in and 20.5 in length. The thruster has a total mass of 6.44 kg (includes engine and valves), with a specific impulse of 215 to 223 sec and a thrust of 440 to 614 N (steady state).

Properties

Overview

Name
MR-104J 440N
Supplier
L3Harris Aerojet Rocketdyne
Type
Other
Flight proven
Yes

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