HP250 Thruster
Agile Space Industries
The HP250 is a bipropellant thruster using N2H4/MON3, designed to be used as axial thrusters for midsize to large spacecraft. Delivering 250 N of thrust, the HP250 is suited for primary propulsion, orbit raising, and significant delta-V maneuvers on larger spacecraft platforms.
About
The HP250 is a bipropellant thruster using N2H4/MON3, designed to be used as axial thrusters for midsize to large spacecraft. Delivering 250 N of thrust, the HP250 is suited for primary propulsion, orbit raising, and significant delta-V maneuvers on larger spacecraft platforms.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
