๐จ๐ณ Cai Hong-4B (CH-4B, reg. AD-34) MALE UAV with visible airborne (C?-Band), datalink antenna, gimballed EO-system and 4 pylons with no mounted carriage.
The ๐จ๐ณ CH-4B MALE UAV is the armed variant of the CH-4 (with the -A version being solely for reconnaissance purposes) developed by CAAA, which is part of CASC.
The drone changed dramatically in terms of aerodynamic design compared to it's predecessor, the CH-3; higher lift-to-drag and aspect ratios with V-shaped tail > lower fuel consumption and more endurance. Most of the body is made of alluminium alloy (with the exception of radome).
The drone has a retractable landing gear system equipped with a hydraulic shock adsorber (also used in the ๐ฎ๐ท Gaza/Shahed-149 UAV) and is propelled by a ๐ฆ๐น Rotax 914 (114 hp/84 kW) 4-cylinder piston engine.
The drone has 4 composite pylons with the ability to carry ๐จ๐ณ AR-1 and ๐จ๐ณ FT-9 guided munitions; both of them spotted to be in use by ๐ฉ๐ฟ Algeria.
Frames from the EO-system; the first in normal mode and the second in IR mode.
Specifications (๐จ๐ณ CH-4B for ๐ฉ๐ฟ Algeria):
Length: 8.5 m
Wingspan: 18 m
MTOW: 1330 kg
Payload: 345 kg
Endurance: 35-40 hrs
Range: 250 km (within LOS), 2000 km (SATCOM)
Cruise altitude: 23,000 ft
Cruise speed: 180 km/h
They were presumably taken by the ๐จ๐ณ YY-12HD EO-system, specifications:
Diameter: 450 x 660 mm
Optical recognition range: +13 km
IR target recognition range: +18 km
Laser rangefinder (LRF): +15 km
Weight: ~60 kg
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Venezuela's first armed UAV: ๐ป๐ช ANSU-100, which is an upgrade to their ARPA program (locally produced ๐ฎ๐ท Mohajer-2) with fixed wheel chassis, making it the first country in South America to possess armed drones.
The ๐ฎ๐ท Mohajer-2 shares the same cylindrical fuselage, twin-boom tails and straight wings as it's predecessor (Mohajer-1). The use of skids instead of landing gear makes it dependent on pneumatic rail launchers. There are 2 known skid designs, of which one is for without EO optic
There are also 2 known engine types installed on the drone; ๐ด๓ ง๓ ข๓ ฅ๓ ฎ๓ ง๓ ฟ WAE-342 (26hp) and ๐ฉ๐ช L-275 (25hp). The ๐ป๐ช ARPA program, from which the ANSU-100 is developed, has the EO-system version (with the associated skid design) and WAE-342 engine type.
#Throwback to when ๐ป๐ช Venezuela showcased it's first light trainer aircrafts: the Simรณn Bolรญvar 100 and 200 (SIBO 100/200), which are locally built ๐ฎ๐ท Iranian Fajr F.3-B and Fajr F.20. #avgeeks
The Fajr F.3-A/B is an all-composite 4-seater single-engine piston aircraft intended for pilot training and light transport. It is powered by a ๐บ๐ธ Lycoming AEIO-540-L1B5 6-cylinder piston engine (300 hp/220 kW) with a 3-blade ๐ฉ๐ช Hoffmann propeller. The -A has a fixed landing...
...gear while the -B has a retractable one. The flap system is of Fowler-type and the use of composites for the Fajr F.3 structure has increased the overall strength while reducing weight. An emergency gear extension system has been installed in addition to the main extension.