200 N HPGP RCS Thruster
bradford-space-ecaps
Reaction control system configuration of the 200 N HPGP monopropellant thruster for high-thrust attitude and orbit control.
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 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.
