SW
The Future of Aerospace
We conquer the sky with high tech drones that fly long-range and hours without losing power or strenght in signal.
Project blueprint
What makes us better than everyone else?
The system is based on 20 years of knowledge and experience. Back in 2003, the StratoWave team was practically among the first in the world to broadcast a sailing regatta live on-line. Half a year later, also in 2003, the first plane in Croatia was connected to the Internet and the first ever email from the air over Zagreb was sent from it, and it was accompanied by a livestream.
That’s just the beginning of our story.
Long-range
The system has been tested several times in real conditions and has been proven to operate at 50 km.
HYBRID DRIVE
Electric propulsion is a supplement that controls practically direct transmission of power from the central engine for each individual propeller in the multirotor configuration of the aircraft.
Internal combustion
A hybrid system refers to an integrated semi-direct drive consisting of a central internal combustion engine and an electric drive unit.
ENERGY EFFICIENT
Because the specific energy density of fuel (depending on the internal combustion engine used) is 20-30 times higher than today’s batteries for electric drones, the autonomy is increased practically as many times.
Long-range
The system has been tested several times in real conditions and has been proven to operate at 50 km.
HYBRID DRIVE
Electric propulsion is a supplement that controls practically direct transmission of power from the central engine for each individual propeller in the multirotor configuration of the aircraft.
Internal combustion
A hybrid system refers to an integrated semi-direct drive consisting of a central internal combustion engine and an electric drive unit.
ENERGY EFFICIENT
Because the specific energy density of fuel (depending on the internal combustion engine used) is 20-30 times higher than today’s batteries for electric drones, the autonomy is increased practically as many times.
ABOUT
Internal Combustion
Expected performance of the prototype aircraft in the development phase:
Maximum take-off mass MTOW = 25 kg
Quad-rotor X configuration
Propellers: 27 “
Internal combustion engine power: 6 kW
Maximum peak hybrid power: 12 kW
Expected autonomy without load (maximum amount of fuel): 8-12 hours
Maximum share of payload in relation to MTOW: 30%
about
Communication systems
The features of the system are:
C Band
MiMo 4x4 technology
Circular Polarization (2xLHCP + 2xRHCP)
33 dBm (2 W)
Predicted data speed:
about 1 km ≤ 500-700 Mbit
about 10 km ≤ 200-400 Mbit
100 km ≥ 10-40 Mbit (expected projection after path loss)
Bandwidths: 20, 40 and 80 MHz
Communication protocol: TCP / IP
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