200N Monopropellant Hydrazine Thruster
Rafael Advanced Defense Systems - Space Division
The Rafael 200N Monopropellant Hydrazine Thruster is a high-thrust space propulsion unit designed for integration into Roll Attitude Control System (RACS) clusters for satellite launchers. Each RACS cluster integrates the 200N thrusters with valves, pressure transducers, manifolds, and an electronic driver to form a complete attitude control assembly. The thruster delivers 200 N ±5% steady-state […]
About
The Rafael 200N Monopropellant Hydrazine Thruster is a high-thrust space propulsion unit designed for integration into Roll Attitude Control System (RACS) clusters for satellite launchers. Each RACS cluster integrates the 200N thrusters with valves, pressure transducers, manifolds, and an electronic driver to form a complete attitude control assembly.
The thruster delivers 200 N ±5% steady-state thrust with a specific impulse exceeding 220 seconds. The single-coil, single-seat NC solenoid FCV provides rapid response with rise time under 150 ms. The nozzle expansion ratio is 50:1.
Flight heritage with the Israeli satellite launcher program. Manufactured to ISO 9001:2015 / AS9100D and ITAR-free.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
