1 N HPGP Thruster
Bradford Space
Flight-proven HPGP monopropellant thruster delivering 0.25-1 N thrust, used for AOCS and delta-V on CubeSats to smallsats.
Typed specifications6 values
Discloses 4 of 10 fields engineers filter by in this category (category median 3).
- Mass
- 390 g product page
- Thrust
- 250–1 000 mN product page
- Specific impulse
- 204–231 s product page
- Propellant
- LMP-103S (ADN) product page
- Power consumption
- 12 W product page
- Feed / tank pressure
- 5.5–22 bar product page
Each value is typed with its unit and measurement condition and cites the datasheet page it was taken from. Nothing is guessed: a field that is absent here has not been published by the manufacturer. machine-extracted ✓ checked by NewSpace Market ✓ manufacturer confirmed by the manufacturer.
As published by the supplier8 lines, in the manufacturer's own wording
- 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.