200 N HPGP Thruster
bradford-space-ecaps
High-thrust HPGP monopropellant engine delivering 50-200 N for reaction control system (RCS) applications.
Technical specifications
- 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.
