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Scout B1-100 UAV system

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Aeroscout Scout B1-100 UAV

Autonomous Industrial Unmanned Helicopter

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 30 kg (incl. 10 l of fuel (standard), 4 kg flight control system FCS) with an empty weight about 45 kg (MTOW 75kg, depending on flight altitude above mean sea level).

SAFETY The helicopter has been developed under severe safety policies, high engine power reserve capacities, mechanic robustness (multiple load excess), and environmental robustness 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 100ccm 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 GPS waypoint (position) mode.

DEMONSTRATION System demonstrations are available on request in Lucerne, Switzerland.

INFORMATION For further information please contact Aeroscout GmbH, Switzerland.

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TECHNICAL DATA
Main rotor diameter 3.2 m
Tail rotor diameter 0.65 m
Main rotor speed 860 rpm
Empty weight (no fuel, no payload) 45 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)
STANDARD PAYLOAD DATA (500m AMSL)
  • Autonomous INS/GPS flight control system (approx): 3.0kg (incl. redundant manual backup control)
  • redundant FCS batteries and starter battery (approx.): 1.0kg
  • 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 differential 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 (500m AMSL)
 
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