22N HPGP

Overview

Bradford ECAPS's 22N HPGP Thruster is designed for attitude, trajectory and orbit control of larger satellites and for systems such as propulsive payload adaptor rings.

The 22N HPGP thruster is currently undergoing a test fire campaign with the NASA Goddard Space Flight Center, characterizing the performance of the thruster. This is intended to prepare the 22N HPGP thruster for use on future NASA missions, such as observatory or interplanetary science missions.

Specifications

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