MR-103G 1N

MR-103G 1N image unavailable

Overview

MR-103G 1N is a flight proven hydrazine monopropellant thruster. The thruster has a total mass of only 0.33 kg, with a specific impulse of 202 to 224 sec and a thrust of 0.19 to 1.13 N (steady state).

Specfiications

Form Factor
SmallSat
Heritage
Yes
Dry Mass
0.33 kg
Average Power
16.11 W
Status
In Production