Safety is our priority
Redundancy at every level: power, navigation, control, communication
01
Power redundancy – two independent 28S channels.
02
Sustained flight with one motor failure
03
Hands‑free hover and emergency landing functions
04
Dual GPS RTK + EKF3 – centimetre precision
05
Whole‑airframe ballistic parachute system
06
Radar‑based auto‑landing system
Failsafe Scenarios
Scenario
System response
Loss of RC link
Automatic return to launch point and landing
Critically low battery
Pilot warning, automatic landing
Single motor failure
Thrust redistribution to remaining 7 motors
GPS/navigation loss
Switch to optical flow (H‑Flow) and barometric mode
Flight controller failure
Backup controller triggers auto‑land
Certification & Compliance
FAA Part 103
Classified as an ultralight vehicle (when mass ≤ 115 kg)
EASA SC‑VTOL
Alignment with special condition for VTOL aircraft
ISO 9001:2024
Quality management system in production
Test status
✓
Hover tests
✓
Single motor failure in flight
✓
Parachute deployment tests
⏳
EASA certification flights
⏱️
Real weather trials