Product Introduction:
The HWA-ZC unmanned aerial vehicle has developed a series of large fixed wing unmanned aerial vehicle models with a conventional fixed wing double tail support layout, supporting two takeoff and landing modes: sliding takeoff and landing and vertical takeoff and landing. It supports carrying multiple mission payloads and is equipped with GPS+Beidou high-precision positioning system, with excellent reliability and anti-interference safe flight capabilities.



HWA-ZC drone three view
The main technical specifications of HWA-ZC unmanned aerial vehicle are as follows:
wingspan |
4.7m |
length |
2.07m |
Standard takeoff weight |
24kg |
Maximum takeoff weight |
30kg |
Maximum mission payload weight |
6kg |
Takeoff method |
Taxiing takeoff/Vertical takeoff |
Takeoff method |
Sliding Landing/Vertical descent |
departure time |
20s |
Power and Capacity |
Oil electric hybrid gasoline92#6L battery6S 5300Mah × 4 (compliant with 3C certification) |
endurance |
10h(3Kg load) |
minimum enroute I.F.R.altitude |
true altitude30m |
Maximum takeoff altitude |
altitude4500m |
Flight height limit |
altitude8000m |
cruising speed |
30m/s |
Maximum flight speed |
40m/s |
Maximum flight distance |
Not less than1000km |
Ground air measurement and control radius |
data radio50km 4G model coverage area: unlimited |
Navigation method |
Beidou+Inertial integrated navigation |
Rainproof ability |
Light rain environment(≤ 10mm/24h) safe flight |
Dimensions |
1800mm×600mm×700mm |
mode of transport |
Support land, sea, and air transportation |
