| Flight System | |
|---|---|
| Type | V-shaped Octocopter |
| Size | 768x817x160mm |
| Engines | 8 electrical, brushless (sensorless) motors with 125W max. power each |
| Rotor Diameter | 8" (~20cm) |
| Number of rotors | 8 |
| Rotor weight | 6g |
| Empty weight | 1.2kg |
| Payload weight (camera and gimbal) | 0.8kg |
| Take off weight | 2.8kg |
| Flight time | Up to 16-2 6mins |
| Max data link range | 1km+ |
| Max altitude | 4,000m MSL |
| Max video link range | 1km+ (FCC version) |
| Max tolerable wind speed | 12m/s (GPS mode) 16m/s (Height mode, Manual mode) |
| Power supply | 2x IntelĀ® Powerpack 4000 (redundant setup) |
| Navigation Sensors | |
| AscTec* Trinity Control Unit | Triple redundant Inertial Measurement Unit (IMU: barometer, compass, accelerometers, gyroscopes) |
| Global Navigation Satellite System (GNSS) | GPS and GLONASS |
| Performance | |
| Max Airspeed - Manual Mode | 18m/s |
| Max Airspeed - Height Mode | 18m/s |
| Max Airspeed - GPS Mode | 4.5m/s standard/ up to 10m/s in mapping flights |
| Climb/sink rate - Manual Mode | 6 to 10m/s |
| Climb/sink rate - Height Mode | 3m/s |
| Climb/sink rate - GPS Mode | 3m/s |
| Turn rate - Manual Mode/Height Mode | 115 degrees/s |
| Turn rate - GPS Mode | 75 degrees/s |
| Wireless Communication | |
| Control Links | Two independent (diversity) command and control links - 2.4GHz adaptive FHSS link 100mW |
| Digital video link | Low latency digital link. 5.1GHz with up to 250mW. Resolution depending on payload, up to 1080p full HD |
|
Data source |
https://www.intel.com/content/www/us/en/drones/falcon-8-drone-brief.html |
Generated using dronespec.info
Source data acquired 2023-02-05 10:09:05