Search...
UUAVSale

"Agile-I" Unmanned Helicopter System(MJ-Ⅰ)

SKU: MD-P00105·UAV Platforms·Made to Order

"Agile-I" Unmanned Helicopter System(MJ-Ⅰ)
"Agile-I" Unmanned Helicopter System(MJ-Ⅰ)
"Agile-I" Unmanned Helicopter System(MJ-Ⅰ)

Overview

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

Technical specification

Specifications. Key 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.

Technical specification — 1 groups
Key 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.

Technical specifications

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

Documents