250N Monopropellant Thruster

250N Monopropellant Thruster image unavailable

Overview

A 225 N monopropellant engine developed by Space Solutions. The thruster the propellant H2O2, has a mass of 0.85 kg, and a specific impulse of 170 seconds.

Specifications

Form Factor
SmallSat
Dry Mass
0.85 kg
Average Power
N/A
Heritage
N/A
Status
In Production