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Overview

MR-501 0.09N is a flight proven hydrazine monopropellant thruster. The thruster has a total mass of 0.60 kg, with a specific impulse of 180 to 184 sec (steady state) and a thrust of 0.07 to 0.09 N (steady state).

Properties

Overview

Name
MR-401 0.09N
Supplier
L3Harris Aerojet Rocketdyne
Type
Other
Flight proven
Yes

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