Camflight FX8 Multirotor UAS

fx8

    • Up to 50 min. flight endurance for coverage of large areas
    • Needed space for takeoff and landing: 3 x 3 meter
    • Autopilot from Lockheed Martin for high precision flights
    • High stability in wind
    •  Virtual cockpit ground control software for advanced flight plans
    • Short time from arrival to airborne
    • Stabilized brushless camera gimbal
    • Flight case for protected transportation
    • 40 A fast charging system
  • Vertical Takeoff / Land multi-rotor electric aircraft, commercial-grade

     

     

    Physical:
    Size: < 140 cm diameter, ~ 45 cm height.
    28” / 29” two blade propellers
    Weight: < 24,75 Kg including maximum payload
    Battery – 44 000 mAh 8S - 29,6 V
    Speed: – 15 m/s
    Payload: Swappable EO / IR / HD with real time downlink Avionics/GCS: Lockheed Martin Procerus Kestrel Autopilot v3.1 & Virtual Cockpit GC software

     

    Environmental:

    Max Wind: ~12 m/s
    Moisture: Light Rain-
    Temperature: -20 → 40 Degrees Celsius

     

    Communications:

    Communication Frequency 2400 MHz (other frequencies optional)
    (digital video link optional)
    Max Communication Range 2 km (depending on frequency)

     

    The Failsafe Behaviors are: (user configurable in the Virtual Cockpit GCS)

    loss of RC Comm 0.5 sec -> fly level
    loss of RC Comm 2 sec -> fly to the rally point loss of Comm 3 sec -> fly to rally point
    loss of Comm 10 sec -> land at the land point loss of GPS 2 sec -> fly level
    loss of GPS 10 sec -> land at current location low battery 3 sec -> land at land point
    critically low battery -> land at current location
    If multiple failsafes are triggered the failsafe behavior with the highest priority will be implemented. The failsafe priority in order of highest to lowest is:
    1) critically low battery 4) low battery
    2) loss of GPS 5) loss of RC Comm
    3) loss of Comm

     

    Payload & Endurance:

    Max Payload Capacity: 8200 gr.
    Flight Endurance @ 8200 gr. Payload: 25 Minutes to first failsafe stage
    (depending on weather and wind conditions)

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