cabatli_53
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TAI HÜRKUŞ Basic Trainer / COIN Aircraft
HÜRKUŞNew Generation Basic Trainer (HÜRKUŞ) Development Program contract was signed between the Undersecretariat for Defense Industries and TAI in March 2006. HÜRKUŞ with day and night mission capability; instrument flight, navigation and formation training phases will be realized.
Within the framework of the program; two aircraft configurations are being developed.
- HÜRKUŞ-A: Basic version which is to be certified with EASA according to CS-23 requirements.
- HÜRKUŞ-B: Advanced version with integrated avionics (including HUD, MFDs, and Mission Computer).
Stability and control checks in different flight configurations have been conducted in the following flight tests. Landing gear up-down tests, cockpit pressurized tests and system functions pre-checks have been performed. The aircraft has reached 12.500 ft height and 158 knots speed currently. The flight tests are still ongoing.
The first prototype has performed 106 flight-hours in 98 sorties. During these flights;15.000 ft altitude, 295 knot speed and 4.4g values have been tested.
The second prototype with TC-VCI tail number has performed it's first flight on 10 September 2014. During the tests performed so far; 25.000 ft altitude and 234 knot speed values have been tested.
As a resolution of SSIK's meeting, held on Sept. 26, 2013, in order to meet the 15 new-generation trainer aircraft requirement of TurAF, contract negotiations regarding the serial production of HÜRKUŞ was started with TAI. The negotiations regarding HÜRKUŞ-B contract is on the signing stage currently.
Design Features:
- Superior aerodynamic performance, TAI designed wing airfoil
- 1,600 shp PT6A-68T Pratt & Whitney Canada turboprop engine
- Five bladed aluminum Hartzell HC-B5MA-3 propeller
- Martin-Baker Mk T-16 N 0/0 ejection seats
- Inverted Flight
- Good visibility from both cockpits, 50 down-view angle from rear cockpit
- Comfortable accommodation of wide range of pilot sizes
- Pressurized cockpit (nominal 4.16 psid)
- On-Board Oxygen Generating System (OBOGS)
- Anti-g System
- Environmental Control System (Vapor Cycle Cooling)
- Strengthened canopy for bird strike resistance
- High shock absorbing landing gears for training missions
- Hands On Throttle and Stick (HOTAS)
Maximum Cruise Speed310 KCAS (574 km/h)
Stall Speed (landing configuration)77 KCAS (143 km/h)
Maximum rate of Climb (@ sea level)4370 ft/min (22 m/s)
Service Ceiling34700 ft (10577 m)
Maximum Endurance (@15,000 ft)4 h 15 min
Maximum Range (@15,000 ft)798 n mile (1478 km)
Total Take-Off Distance (@ sea level)1605 ft (489 m)
Total Landing Distance (@ sea level)1945 ft (593 m)
g limits+7 / -3,5g
*Values given in the table are calculated under International Standard Atmospheric (ISA) conditions.
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After Anka MALE UAV, MSB Vecdi Gonul announced that TAI has almost finished the Production/Assembly of Hurkus Basic trainers and Roll-out would be performed in a short time...
?lk Türk uça?? hangardan ç?k?yor
According to TAI officials, Hurkus will be produced in two different category.
Hurkus A-Acbobatic turpoprop
Hurkus B-Military trainer/ COIN missions
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