MRM-122 130N

MRM-122 130N image

Overview

MRM-122 130N is a flight proven hydrazine monopropellant thruster. The thruster has a specific impulse of 217 to 228 sec and a thrust of 51 to 142 N (steady state).

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Overview

Name
MRM-122 130N
Form Factor
SmallSat
Heritage
Yes

Vendor Details

Name
Aerojet Rocketdyne
Founded
1942

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Specifications

Form Factor
SmallSat
Dry Mass
N/A
Average Power
43.0 W
Heritage
Yes
Status
In Production
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