200 N HPGP Thruster
Bradford Space
High-thrust HPGP monopropellant engine delivering 50-200 N for reaction control system (RCS) applications.
Key figurescomparable across the catalogue
- Mass
- 5.7 kg
- Power
- 150 W
- Thrust
- 50 N
- Specific impulse
- 206 s
Normalised to common units so this product can be compared with others in its category. The supplier's own wording is below.
As published by the supplier
- 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.