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Overview

MR-104H 510N is a flight proven hydrazine monopropellant thruster. The thruster has a total mass of 2.40 kg (includes engine and valves), with a specific impulse of 223 to 237 sec and a thrust of 201.0 to 554.2 N (steady state).

Properties

Overview

Name
MR-104H 510N
Supplier
L3Harris Aerojet Rocketdyne
Type
Other
Flight proven
Yes

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