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.
The ๐ฎ๐ท Mohajer-2 has optional weapon equipment; an already known example of which is two six-round ๐ท๐บ PG-7V/๐ฎ๐ท Fath (RPG-7 rockets) launchers. The weight of this payload would deem the use of ๐ฎ๐ท Qa'em-5 bombs possible, as shown alongside the ๐ป๐ช ANSU-100.
The ๐ป๐ช ANSU-100 has a non-retractable wheel chassis, which causes additional drag but makes take-off on (paved/unpaved) runways possible. It's design is distinguishable to the Iranian variant.
There are no available ๐ป๐ช ANSU-100 UAV specifications yet but if we assume upgrades undertaken to be within the range of ๐ฎ๐ท Mohajer-2N standard:
Length: 2.91 m
Wingspan: 3.82 m
MTOW: ~90-105 kg
Speed: ~180 km/h
Range: ~100-150 km
Endurance: ~4-6 hrs
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).
#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.