SAFETY MEASURES
Redundancy Systems
The dual-bus power architecture independently supplies all eight motors, ensuring stable output even if one power source fails.
Every critical component on the HayesX-250 — from propulsion to control — is designed with multi-layer redundancy to ensure reliability under any condition.
A dual-IMU (Inertial Measurement Unit) gyroscopic system and dual-control bus continuously cross-verify flight data in real time, maintaining full flight control integrity. Even if a rotor or subsystem fails, the aircraft remains controllable and can perform a safe, stable descent, safeguarding the pilot.
Equipped with the world’s most advanced whole-aircraft parachute rescue system, our aircraft can safely deploy its ballistic parachute from as low as ten meters above the ground, providing unparalleled critical protection in low altitude emergency situations.
The dual-bus power architecture independently supplies all eight motors, ensuring stable output even if one power source fails.
Every critical component on the HayesX — from propulsion to control — is designed with multi-layer redundancy to ensure reliability under any condition.
A dual-IMU (Inertial Measurement Unit) gyroscopic system and dual-control bus continuously cross-verify flight data in real time, maintaining full flight control integrity. Even if a rotor or subsystem fails, the aircraft remains controllable and can perform a safe, stable descent, safeguarding the pilot.
Other Key Safety Measures
Every flight is built on the promise of protection, reliability, and peace of mind.
Emergency Assisted Landing System: An integrated emergency landing control function with radar sensors enables stabilized descent and automatic landing in abnormal conditions.
Motorsport-Grade Roll Cage Protection: Based on motor racing safety standards, the special design of high-strength roll cage structure ensures pilot protection even under extreme impact scenarios.
Distributed Propulsion Fault Tolerance: With an eight-motor distributed propulsion system, the aircraft remains controllable in the event of a single motor failure, allowing for safe return or controlled landing.
Emergency Power Cut-Off Systems: Critical safety mechanisms are designed to isolate electrical systems during emergencies. These systems are highly redundant to rapidly terminate hazardous conditions.