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Agile-I Helicopter Drone Military Autonomous Landing For Fire Detection
  • Agile-I Helicopter Drone Military Autonomous Landing For Fire Detection
  • Agile-I Helicopter Drone Military Autonomous Landing For Fire Detection

Agile-I Helicopter Drone Military Autonomous Landing For Fire Detection

Place of Origin China
Model Number "Agile-I"
Product Details
Highlight: 

Autonomous Landing Helicopter Drone Military

,

Fire Detection Helicopter Drone Military

,

Fire Detection Fire Scout Helicopter

Payment & Shipping Terms
Minimum Order Quantity
1 Set
Packaging Details
Carton
Delivery Time
Peak Season Lead Time: one month Off Season Lead Time: one month
Payment Terms
LC, T/T, D/P, PayPal, Western Union
Product Description
Description
About The "Agile-I" Unmanned Helicopter System(MJ-Ⅰ)
China Electronics Technologies Group
"Agile - Ⅰ" is a kind of intelligent small unmanned helicopter system, the machine has good flight performance, has the over-the-horizon autonomous flight, autonomous landing, fixed-point hover, flights, a key homing, and other functions, can realize the regional reconnaissance, fixed-point characterization, target and tracking, etc., is an ideal air access to information platform “

Application:
Geological disaster site investigation ;
Fire detection
Traffic emergency scene investigation ;
Power line patrol ;
Area security monitoring

Development process :
In February 2008, the start "agile - Ⅰ" unmanned helicopter system research work, in February 2009, to complete the whole system function function index, has realized automatic take-off, automatic landing, automatic flight routes, and functionality; In December 2009, the product design was finalized, and the first set of products was delivered to users in May 2010.

System composition:
''Agile -Ⅰ'' unmanned helicopter system is composed of helicopter plat sub-system , measurement and control sub-system, mission payload sub-system and comprehensive security subsystem.

Specifications
  • Length: 1.778 m
  • Height: 0.711 m
  • Rotor diameter: 2.146 m
  • Rotor area: 0.5 m2
  • Empty weight: 15 g without batteries and fuel
  • Fuel: 4 l
  • Normal payload: 5 kg
  • Max take-off weight: 50 kg
  • Max speed: 70 km/h
  • Cruise speed: 60 km/h
  • Rate of climb: 5 m/s
  • Range: 80 km/h
  • Endurance: 80 min
  • Ceiling: 3.5 km

 
 
 
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