MRM-122 130N

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).

Specifications

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