Technical side of HEROS
| Width | 70 in | 1,775 mm |
| Height | 81.9 in | 2,080 mm |
| Fuselage lenght | 184 in | 4,675.5 mm |
| Rotor diameter | 165.75 in | 4,210 mm |
| DOM | 639 lbs | 290 kg |
| Fuel capacity | 30.1 US gal | 114.2 litres |
| Maximum payload | 440.9 lbs | 200 kg |
| MAUW | 1,234 lbs | 560 kg |
| Cruising speed | 75 kts | 139 km/hr |
| Maximum speed | 98 kts | 181 km/hr |
| Maximum endurance | 6 hours | |
| Maximum hovering endurance | 3.5 hours | |
| Range | 155 miles | 250 km |
| Telemetry range | 100 miles | 160 km |
Features
- HEROS has been developed as EASA EASA-CS27/EASA-CSVLR compliant
- A Category A twin-engine helicopter able to operate in 2nd performance class over congested areas
- Co-axial rotor – high effectivity, high stability, broad field of applications
- Long endurance (>4hours of flight)
- Ceiling >4000m MSA
- Professional design and projection
- Helicopter and cargo module interface
- In-flight and landing cameras
- Ballistic recovery parachute
- In-flight and cargo telemetry
- Transponder mode A, C, S
- Surface finish as per customer‘s wish
- Cargo module as per customer‘s specification
- Power – 2 piston engines ROTAX 503 (total output 100 hp)
- Airframe – steel tube construction (L-CM3) with composite fuselage
- Composite landing gear with dural skids
- The UAV is equipped with camera system and IR searchlight
- 12V el. system is powered with 2 generators (155W) and a backup 12 V battery.
- Avionics
- Sense and Avoid
- IFPS – Inertial Flight Position System
- DGPS – Differential GPS
- Altimeter and airspeed indicator
- LASER Altimeter
- Radar/Ladar
- PCU – Pilot Control Unit
- Measuring aparature
- The SSR Transponder
- The UAV is BRS (ballistic recovery system) equipped