1 N HPGP Thruster
bradford-space-ecaps
Flight-proven HPGP monopropellant thruster delivering 0.25-1 N thrust, used for AOCS and delta-V on CubeSats to smallsats.
Technical specifications
- Thrust
- 0.25-1 N
- Specific Impulse
- 204-231 s
- Mass
- 0.39 kg
- Pulse Count
- 60,000
- Feed Pressure
- 5.5-22 bar
- Heater Power
- 12 W
- Function
- AOCS + ΔV
- Propellant
- LMP-103S (ADN-based, non-toxic)
About
The 1 N HPGP thruster from ECAPS (a Bradford Space company) is a flight-proven monopropellant thruster running on the non-toxic, ADN-based LMP-103S propellant. It has flown on multiple missions including the ArgoMoon lunar rideshare mission on Artemis I, using 100 mN and 1 N class thrusters.
The 1 N HPGP delivers reliable attitude control and station-keeping delta-V for CubeSats and small satellites, with high pulse-count endurance suited to long-duration AOCS duty cycles.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
