Intel Falcon 8+ User Manual page 122

Figure 7-1. Technical data
Type
Size
Engines
Rotor diameter
Number of rotors
Rotor weight
Empty weight
Max. payload weight (camera and gimbal)
Max. take off weight
Max. flight time without payload*
Max. flight time with max. payload weight*
Max. flight time with A7R
Max. flight time with Inspection payload
Max. range data link**
Max. service ceiling**
Max. altitude above ground level**
Max. range video link**
Max. tolerable wind speed
Max. precipitation
Operating temperature
Storage temperature
Power supply
AscTec Trinity Control Unit
Global Navigation Satellite System (GNSS)
Manual-Mode
Height-Mode
GPS-Mode
Max. climb/sink rate
Manual-Mode
Height-Mode
GPS-Mode
Max. turn rate
Manual-Mode / Height-Mode
122
The UAV
V-Form Octocopter
768 x 817 x 160 mm
8 electrical, brushless (sensorless) motors with 125 W
max. power each
20.32 cm (8 in)
8
6 g (0.21 oz)
1.2 kg (2.65 lbs)
0.8 kg (1.76 lbs)
2.8 kg
26 min
16 min
16 min
18 min
1 km (FCC version) (3281 feet)
4000 m MSL (13123 feet)
Varies by country in which you operate the UAV and
requires you to check the regulations that apply for
your country of operation
500 m (FCC version) (1640 feet)
12 m/s (26 mph) (GPS Mode)
16 m/s (35 mph) (Hight Mode, Manual Mode)
Not recommended to operate in any form of
precipitation
-5 °C to 45 °C (23 °F to 113 °F)
5 °C to 25 °C (41 °F to 77 °F)
2 x Intel Powerpack 4000 (redundant setup)
Navigation Sensors
Triple redundant Inertial Measurement Unit (IMU:
barometer, compass, accelerometers, gyroscopes)
GPS and GLONASS
Max. Airspeed
18 m/s (40 mph)
18 m/s (40 mph)
4.5 m/s (10 mph) standard
8 m/s in GPS based video mode
up to 10 m/s (22 mph) in mapping flights
6 to 10 m/s (13 to 22 mph)
3 m/s (6 mph)
3 m/s (6 mph)
115°/s
User Manual ®
TM
Intel Falcon F8+