S-30 Duck Layout Unmanned Aerial Vehicle System

▲ The aircraft adopts an advanced canard layout

with better aerodynamic performance, and both

the main and canard wings can generate lift,

greater load capacity;

▲ Aircraft has low aerodynamic resistance and

longer flight hours;

▲ The rotor is installed below the main wing and

above the vertical tail, eliminating the need for

dedicated mounting rods to reduce the weight of the fuselage.

▲ The body is equipped with rotor systems on both sides, which can take off and land vertically in complex terrain environments, or activate the rotor for protective landing in emergency situations;

▲ The power adopts an electronic gasoline injection engine and an onboard electric starting device, which can start in the air without the need for an external starter and is more convenient to use.

Item	Parameters
Wingspan	3.368m
Full height	0.68m
Load weight	10kg
Takeoff and landing mode	Four rotor vertical takeoff and landing
Stall speed	16m/s
Maximum flight altitude	5000m
Maximum battery life	6h
Measurement and control task radius (under visibility conditions)	10-50Km
Navigation mode	GLONASS, BDS
Fuel	92 # and 95 # automotive gasoline

 

▲ The circular cabin has a larger interior and can accommodate larger loads;

▲ The vertical tail can also serve as the main landing gear, eliminating the need for a landing gear, resulting in lighter weight and less resistance;

▲ The body material is carbon fiber, with light weight and high strength. Fiberglass Kevlar material can also be used, with lower RCS, suitable for long-term reconnaissance operations;

Item	Parameters
Length	1.85m
Maximum takeoff weight	34Kg
Body material	Carbon fiber or fiberglass
Cruise speed	22m/s
Max climb rate	3.5m/s
Maximum level flight speed at sea level	30m/s
Maximum wind resistance	Level 5
Flight mode	Fully autonomous, manual
Dynamic system	Two stroke internal combustion engine+ electric starting
Rotor battery	High discharge rate ternary lithium battery