Aeroscout Scout B1-100
Autonomous Industrial Unmanned Helicopter

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GENERAL The autonomous industrial unmanned helicopter Scout B1-100 has been developed for professional airborne applications such as aerial mapping, airborne broadcasting, search & rescue, surveillance and inspection as well as law enforcement.
PAYLOAD The helicopter provides a payload capacity of up to 31 kg (incl. 10 l of fuel (standard), 2 kg flight control system FCS) with an empty weight of only 44 kg (MTOW 75kg).
SAFETY The helicopter has been developed under severe safety policies, high engine power reserve capacities, mechanic robustness (3x load excess), and environmental robust against spray water.
FEATURES The Scout B1-100 provides easy transportability and maintainability through system modularity, flexible payload options, and a smooth and easy-to-start gasoline engine.
OPERATION The helicopter can either be flown in conventional manual mode with high maneuverability or can be operated with its integrated INS/GPS automated flight control system. This flight control system allows joystick (velocity) mode as well as waypoint (GPS) mode.
DEMONSTRATION System demonstrations are available on request in Lucerne, Switzerland.
INFORMATION For further information please contact Aeroscout GmbH, Switzerland.



TECHNICAL DATA
| Main rotor diameter | 3.2 m |
| Tail rotor diameter | 0.65 m |
| Main rotor speed | 840 rpm |
| Empty weight (no fuel, no payload) | 44 kg |
| Gasoline engine | 100 ccm |
| Engine power (approx.) | 18 PS |
| Electric starter (onboard included) | 16V |
| Fuel tank volume (standard) | 2 x 5.0 l |
| Material of rotor blades | carbon |
| Material of body | aluminum |
| Engine cooling system | air-cooled |
| Length | 3.3 m |
| Width | 0.5 m |
| Height (approx.) | 1.0 m |
| Landing gear | skids (wheels optional) |
PAYLOAD DATA
- Autonomous INS/GPS flight control system (approx): 4.0 kg (incl. battery)
- Standard fuel tank (approx.): 9.0 kg
- Free payload capacity (approx.): 18.0 kg
FEATURES
- Air-cooled gasoline aircraft engine with electric starter onboard
- Easy transportability and maintainability through modularity
- Sealed gear boxes and electronics
- Highly reliable mechanical design
- Integrated, autonomous flight control system FCS
- Optional (D)GPS/INS integrated navigation system with accuracy evaluation
- Flexible payload options
- High maneuverability
- Smoothly running engine and optimal vibration isolation of the payload
- Long-term flight endurance up to 90min non-stop

