200 N HPGP Thruster
Bradford Space
High-thrust HPGP monopropellant engine delivering 50-200 N for reaction control system (RCS) applications.
Typed specifications6 values
Discloses 4 of 10 fields engineers filter by in this category (category median 3).
- Mass
- 5.7 kg product page
- Thrust
- 50 000–200 000 mN product page
- Specific impulse
- 206–234 s product page
- Propellant
- LMP-103S (ADN) product page
- Power consumption
- 150–250 W product page
- Feed / tank pressure
- 5.5–24 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
- 50-200 N
- Specific impulse
- 206-234 s
- Mass
- 5.7 kg
- Pulse count
- 2,000
- Feed pressure
- 5.5-24 bar
- Heater power
- 150-250 W
- Function
- RCS
- Propellant
- LMP-103S (ADN-based, non-toxic)
About
The 200 N HPGP thruster from ECAPS (a Bradford Space company) is a high-thrust monopropellant engine running on the non-toxic, ADN-based LMP-103S propellant, designed for reaction control system (RCS) applications requiring substantial impulse bit and thrust levels.
Part of ECAPS’ HPGP thruster family that spans 100 mN to 220 N across orbital, atmospheric and subsea propulsion regimes, with over 350 flight units deployed using LMP-103S propellant.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.