MRM-106F 40N

Overview

MRM-106F 40N is a flight proven hydrazine monopropellant thruster. The thruster has a total mass of 2.23 kg, with a specific impulse of 231 sec and a thrust of 40 N per rocket (steady state).

Specifications

Form Factor
SmallSat
Dry Mass
2.23 kg
Average Power
20.1 W
Heritage
Yes
Status
In Production