SPECIAL UAV MISSIONS
Based on the "HERCULES ONE" and "HERCULES TWO" UAVs Aeroxess is in the position to provide a wide range of flight services for industrial and R&D applications beyond antenna measurements.
Right from the beginning Aeroxess started with the development of own large UAVs, because soon became quiet obvious that the concepts of commercial available multi-rotor drones or UAVs are facing their limits when up-scaling towards larger UAVs to reach longer flight durations at more payload capacities.
The fact that Aeroxess designs, produces, tests and operates their own UAVs is also an excellent prerequisite to customise the HERCULES UAVs for efficient and optimised integration of customer-furnished payloads.
Currently three different HERCULES UAVs are prepared for flight services.
AEROXESS UAV FLEET
UAV Type | HERCULES MICRO (Battery Version) |
HERCULES ONE-T (Tethered Version) |
HERCULES ONE-H (Hybrid Version) |
---|---|---|---|
Abbreviation | N/A | H1-T | H1-H |
Payload (P/L) Capacity | 1,0 kg | 5.0 kg | 5.0 kg |
P/L Power Supply | 50 W | 500 W | 500W |
Flight Duration | 0.1 h | theoretically unlimited |
2.0 h @ 5 kg P/L 6.0 h @ 2 kg P/L |
Max. Take-Off Weight | 3.5 kg | 15 kg | 20 kg |
Overall Dimensions | ∅ 1.0 m | ∅ 2.1 m | ∅ 2.1 m |
No. of Rotors (Frame) | 4 (X4) | 2 x 3 (Y6) | 2 x 3 (Y6) |
No. of Blades/Rotor | 2 | 4 | 4 |
Rotor Diameter | 0.38 m | 0.85 m | 0.85 m |
Thrust Control | Variable Pitch | Variable RPM | Variable RPM |
Rotor Drives | One Single E-Motor for 4 Rotors |
6 E-Motors: One E-Motor per Rotor |
6 E-Motors: One E-Motor per Rotor |
Energy Supply | Electrical Power from Batteries On-Board |
Electrical Power from Ground Power Supply |
Combustion- Engined Generator by 2-Cylinder 4-Stroke 80cc Boxer Engine |
Operation | Tetherless by Battery Power |
Tether by Power Cable |
Tetherless by Hybrid Power |
Safety Features | Auto-Rotation | Emergency Modes at Loss of up to 2 Rotors and at Separation of Ground Cable by Emergency Batteries |
Emergency Modes at Loss of up to 2 Rotors and at Malfunction of Combustion Engine by Emergency Batteries |
Application | Technology Model | Near Line-Of-Sight Operations and Sidewise DUT Operations |
Far Line-Of-Sight Operations and Above- and Sidewise DUT Operations |
Max. Flight Height | 50 m | 50m | 300m |
Status | In Service | Flight Test Phase; In Service: Sping 2019 |
Manufacturing Phase; In Service: 2020/2021 |