Extreme macro detail of a Hall-effect thruster nozzle during active xenon plasma testing, deep space-black background, luminescent blue-purple glow, high-contrast technical studio lighting.
Extreme macro detail of a Hall-effect thruster nozzle during active xenon plasma testing, deep space-black background, luminescent blue-purple glow, high-contrast technical studio lighting.
/ FLIGHT-QUALIFIED PROPULSION

Flight-qualified Hall-effect thrusters.

Standardized electric propulsion systems engineered for rapid spacecraft integration, offering flight-qualified reliability and high-throughput manufacturing for commercial and defense satellite constellations.

■ ENGINEERING DATA

Performance metrics

Rigorous telemetry and physical dimensions verified through extensive thermal-vacuum testing cycles. Built for direct integration with standard satellite buses.

THRUSTER UNIT
POWER SYSTEM
FLOW CONTROL

Orbion Aurora

Processing Unit

Propellant Feed

Delivers up to 80 millinewtons of thrust utilizing high-efficiency xenon propellant. Optimized for orbit raising and station keeping.

Automotive-grade power processing unit designed to regulate discharge voltage with minimal thermal dissipation.

Proportional flow control valves ensuring precise xenon delivery to the anode and cathode under varying thermal profiles.

Nominal Power: 1.2 kW Specific Impulse: 1500 s Total Impulse: 1.8 MN-s

Input Voltage: 28V / 100V Efficiency: >93% Mass: 3.8 kg

Feed Pressure: 2.0 bar Flow Accuracy: ±1% Dry Mass: 1.1 kg

▸ CONSTELLATION READY

Access telemetry data

Rapid spacecraft integration

Download complete mechanical drawings, electrical interfaces, and qualification test reports for the Aurora thruster line.

Our systems ship with fully documented telemetry interfaces, standardized mechanical mounting points, and comprehensive CAD models to accelerate your launch timeline.