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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

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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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