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Maximum performance and reliability
A perfect fit for high-precision data acquisition, with multi-payload capacity and performance at elevations exceeding 6,500 meters.
GEOX operates reliably in harsh weather conditions, delivering successful photogrammetry, topography, and magnetometry missions across multiple industries. Our advanced flight platform and specialized sensors enable the secure transport of high-value payloads.
60 min
Maximum flight time
without payload
7 kg
Maximum load capacity
up to
25 Mi
Maximum linear flight
@ 200 m s.n.m. *
12 kg
Total weight
Batteries included
74.5 Mi/hr
Maximum speed
Subject to weather conditions*
37.2 Mi/hr
Wind resistance
up to
8,000
Maximum flight altitude
(m a.s.l)
6,500
Maximum operating altitude
(m a.s.l.)
Auto
Autonomous operations
out of visual range and offline
GPS
Integrated PPK system
GPS/Glonass/Galileo/BeiDou
74.5 Mi/hr
Efficient operation in rainy weather
up to
37.2 Mi/hr
Landing and takeoff
uneven and inclined surfaces



Model
GEOX
Configuration
Engines
Quadcopter
4
Performance
Performance
Maximum flight time*
-
Without payload
-
5 kg
-
10 kg
-
15 kg
Maximum payload capacity
Weight with batteries
Maximum takeoff weight
Maximum flight altitude
Maximum operating altitude
Maximum linear flight*
Maximum speed km/h
Operating temperature
-
Minimum
-
Maximum
Wind resistance
Rain resistance
Landing and takeoff
75 min
40 min
-
-
8 kg
12 kg
20 kg
26,247.2 ft a.s.l.
21,325.5 ft a.s.l.
31 Mi
75 Mi/hr
-11°C
46°C
60
25 mm/h
Inclined surfaces up to 25°
Characteristics
Features
Weight with batteries
Shaft diameter
Unfolded diameter
Propeller size
Propeller material
Propeller type
12 kg
1,200 mm
1,800 mm
28 inCarbon fiber and aviation aluminum Two-blade - Carbon fiber with HD foam core
Communications
Communications
Positioning System
Radio Control
Radio Range
PPK System
Real-Time Video
GPS/Glonass/Galileo/BeiDou
Digital + Vídeo
10 km con enlace de video y telemetría
Integrado
Según payload
Electrical system
Sistema eléctrico
Engine
Total thrust
Power-to-weight ratio
Operating voltage
Maximum battery configuration
Batteries per flight
4 engines
52 N
2.6
50
54,000 mAh
2 o 4
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