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.
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 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.