"Agile-I" Unmanned Helicopter System(MJ-Ⅰ)
SKU: MD-P00105·UAV Platforms·حسب الطلب



نظرة عامة
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 Geological disaster site investigation ; Traffic emergency scene investigation ; 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. ''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. Empty weight: 15 g without batteries and fuel Max take-off weight: 50 kg
المواصفات التقنية
Specifications. المواصفات الرئيسية: Length 1.778 m، Height 0.711 m، Rotor diameter 2.146 m، Rotor area 0.5 m 2، 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.
المواصفات التقنية — 1 groups
المواصفات الرئيسية: Length 1.778 m، Height 0.711 m، Rotor diameter 2.146 m، Rotor area 0.5 m 2، 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.
المواصفات الفنية
Specifications
- Length
- 1.778 m
- Height
- 0.711 m
- Rotor diameter
- 2.146 m
- Rotor area
- 0.5 m 2
- 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