Development
The A/F X program began in 1982 along with the development of what would become the F-22. The criteria for the program was a long range, fast, and maneuverable 5th generation fighter and attack aircraft that could replace the A-7 Corsair, A-6 Intruder, and F-14 Tomcat in the Topsailian Navy and the F-111 Aardvark and F-117 Nighthawk in the Topsailian Air Force. By 1988 two competing designs had been laid down, a swing wing design from Red Wolf Aerospace and a diamond shaped wing design from Northrop Grumman. The Red Wolf Aerospace design was labeled the YF-24 and the Northrop Grumman design was named the YF-23. Several prototypes of both designs had been completed by 1993, and the two aircraft could finally compete head on. Almost immediately the YF-24 showed it's superiority to the YF-23. Although they were tested to both be able to achieve Mach 1.8+ at altitude, the YF-24 was shown to be far more agile and able to carry a larger payload of over 9,000 kg, 1,000 kg greater than the YF-24's 8,000 kg payload. The YF-24 was also shown to have a wider combat radius, 1,100 km compared to only 800 km. The YF-24's variable sweep wings also gave it higher speeds and maneuverability at higher speeds with wings swept and more stability and payload capacity with open wings. In 1996 the Topsailian Military chose the YF-24 design for production. The design was continually refined and the aircraft entered production in 2005. The first aircraft entered service with the TAF in June 2006 and in the Topsailian Navy in February 2007. Since then 510 aircraft have been produced, 260 for the Navy and 250 for the Air Force, and there are plans to produce 300+ more for the Topsailian Military.
STATS:
General Characteristics:Crew: 2
Length: 19.41 meters
Wingspan: 19.1 meters open, 11 meters swept
Height: 5.3 meters
Wing Area: 59.2 m2
Empty Weight: 19,340 kg
Loaded Weight: 31,000 kg
Max Takeoff Weight: 38,900 kg
Powerplant: 2 P-90/C1 Turbofans with supercruise, afterburning, and light thrust vectoring
Dry thrust: 98.4 kN each
Thrust with afterburner: 160.2 kN each
Thrust vectoring: ±10° at 30° per second in pitch and yaw
Performance:Maximum Speed: Mach 1.9 (wings swept) at altitude, Mach 0.99 (wings open)
Range: 3,100 km (unlimited with aerial refueling)
Combat Radius: 1,012 km
Service Ceiling: 22,500 meters
Rate of Climb: 228 m/s
Wing Loading: 340 kg/m2
Electronics:AN/APG-77 radar: 125–150 miles (200–240 km) against 1 m2 (11 sq ft) targets (estimated range)
AN/AAR-56 Missile Launch Detector (MLD)
AN/ALR-94 radar warning receiver (RWR): 250 nmi (463 km) or more detection range
MJU-39/40 flares for protection against IR missiles
Armament:1 GAU-22/A 25 mm Gatling Cannon mounted internally with 280 rounds (can be switched out with M-61 Vulcan and most other western and some Russian guns)
1 large internal bomb bay for either 8 air to air missiles or 4 large ground attack weapons (or mixture of the two)
2 side bays for 4 air to air missiles
2 external hard points for 4 air to air missiles or 2 ground attack weapons or 2 electronic warfare pods
VARIANTS-F/A-24A: Standard Land Variant
-F/A-24N: Naval Variant
-E/A-24: Electronic Warfare Variant
-TiK-24A: Variant Produced by Topsail-Kathmandue Aircraft (identical to F/A-24A)
-TiK-24N: Identical to F/A-24N
-TiK-24E/A: Identical to E/A-24
COST: 130 MILLION NSD PER UNIT.
DPR: 28 BILLION NSD (75 billion NSD for DPR to all 3 variants)
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