200N HPGP (Short)

Overview

Bradford ECAPS's 200N HPGP Thruster is designed for launch vehicle upper-stage reaction control and potential defense applications, such as missile defense. Much of the work into the 200N HPGP has been to investigate potential uses on various launch vehicle upper stage programs, including the Ariane 5ME, and for various spacecraft orbit-raising applications. This thruster is currently in development and looking for partners to bring the prior work into fruition.

Specifications

Form Factor
SmallSat
Dry Mass
5.7 kg
Average Power
200.0 W
Heritage
N/A
Status
In Production