Drone H2 – Prometheus UAV

Key parameters

Transponder

ADS-B

MTOM

Maximum
take-off mass

Weight

without
fuel

Tank

for
fuel

Speed

vertical/horizontal
in km/h

Navigation

GPS, GLONASS
BEIDOU i GALILEO

Communication

Coverage
LTE networks

EU regulations

UE 2019/945
UE 2019/947

Dual modem

2 SIM
cards

Video Transmission

maks. Full HD
(optional – encryption)

Security

parachute
LIDAR, RTH

Dimensions

2,2m x 2,2m
x 1,1m

Ingress protection

Norm
IPX4

Wind resistance

Below
20m/sec

Temperature

Optimum operation
from -20°C

Combustion generator

Weight: 3.8 kg
Total power: 2.4 kW continuous
Output voltage: DC 12 S (49V)
Typical fuel consumption: 750 g/kw-h
Fuel: Mixture of: gasoline 95 + oil
(in a ratio of 25:1 or 4%) with a bio-component content of no more than 5%.

Technical specifications

Frame

UAV type	Multirotor
Configuration	Hexacopter
Material	Carbon fibre composite

Size

Unfolded diameter with propellers	2420 mm
Unfolded diameter with closed propellers	1735 mm
Folded UAV diameter	840 mm
Height	930 mm
Transport case [LxWxH]	970 x 840 x 1110 mm
Propellers	30.2 inch folding

Generator

Number of electric motors	6
Electric power generator	2400W 2-stroke fuel injected
Fuel consumption	1.5-2.5 l/h
Fuel	95 petrol + 2T oil mixture (4%)
Fuel tank capacity	9l
Back-up Battery	2 x 6S 4500mAh

Weight

Empty mass (no fuel or payloads)	17 kg
Maximum take-off mass	23 kg
Maximum payload	5 kg + 1kg of fuel

Performance

Maximum flight time without payload*	4-5h
Maximum fligh time with 3kg payload*	2-3h
Flight range	up to 200 km
Maximum speed	90 km/h
Maximum wind resistance	20 m/s
Thrust to weight ratio	2.5:1 for 23kg
Operating temperature	-20°C

Autopilot

Flight modes

Auto, loiter, altitude hold, RTH, land, guided (waypoints)

Control

Communication

Mobile network only. Two independent LTE modems, up to two mobile network operators. Prometheus Dual Modem proprietary redundant data link for command and control. Proprietary live video transmission for main camera and auxiliary cameras. Diagnostic data over network. Payload control and monitoring from GCS.

Equipment

Basic	Front camera, Landing camera, Height LiDAR sensor, Front LiDAR sensor, pyrotechnic parachute, Viewport gimbal connector, Dual GNSS recievers, Redundant compasses
Optional	ADS-B module, RTK positioning system

* depending on conditions

Other elements of the platform