Anka-S UAV 3D model

The model is designed in Solidworks. It includes UAV body, rocket launcher and missile(cirit). Scale:1/1. It is available to print in 3D printer. Available formats: SLDPRT, SLDASM, STP, STL, IGES. Technical support after sales.

The TAI Anka is a family of unmanned aerial vehicles developed by Turkish Aerospace Industries primarily for the Turkish Air Force. Envisioned in the early 2000s for aerial surveillance and reconnaissance missions, Anka has evolved into a modular platform with synthetic aperture radar, precise weapons, and satellite communication.

Anka-S is a serial production configuration of Anka. It is equipped with a SATCOM antenna and a national flight control computer. Like Block A and Block B, Anka-S is powered by Thielert Centurion 2.0S. On the other hand, Turkish Engine Industries (TEI) indigenously developed TEI PD170 and PD180st engines that are capable of running with diesel and JP-8 jet fuel.

**General characteristics Capacity: 350 kg (772 lb) Length: 8.6 m (28 ft 3 in) Wingspan: 17.5 m (57 ft 5 in) Height: 3.25 m (10 ft 8 in) Max takeoff weight: 1,700 kg (3,748 lb) Powerplant: 1 × Tusaş Engine Industries TEI-PD170[84][85] 4-cylinder liquid-cooled in-line turbo-charged diesel engine, 127 kW (170 hp) . Note: Older aircraft use Thielert Centurion 2.0. Propellers: 3-bladed constant-speed propeller Performance

Maximum speed: 217 km/h (135 mph, 117 kn) Cruise speed: 204 km/h (127 mph, 110 kn) Range: 4,896 km (3,042 mi, 2,644 nmi) [86] Combat range: 250 km (160 mi, 130 nmi) datalink range Endurance: 30 hours with 350 kg (772 lb) at mission altitude Service ceiling: 9,144 m (30,000 ft) [87] Avionics ASELSAN CATS, SAR/GMTI, ISAR payload INS/GPS and air data sensor suite system[7] Ctech DEV-KU-18 Mobile Satellite Communication Terminal Armaments MAM (Smart Micro Munition) Roketsan Cirit Tubitak-Sage Bozok Laser Guided Rockets[88][89] L-UMTAS (Long Range Anti tank Missile System)

-Wiki