200 N HPGP RCS Thruster
Bradford Space
Reaction control system configuration of the 200 N HPGP monopropellant thruster for high-thrust attitude and orbit control.
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 RCS Thruster is the reaction control system (RCS) configuration of ECAPS’ (a Bradford Space company) 200 N-class HPGP monopropellant engine, optimized for the pulse-mode operation characteristic of RCS duty cycles on satellites and orbital vehicles.
Running on the non-toxic, ADN-based LMP-103S propellant, it provides high-thrust attitude and orbit control without the toxic handling requirements of hydrazine-based RCS thrusters.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.