ANA Projects

ANA Aircraft

The ANA Modern Fighter Family

The Light Multirole Fighter LMF or Wave FG-1 (Real Life J-10)

Wave FG-1

General characteristics

   * Crew: 1 (basic), 2 (trainer variant)
   * Length: 16.5 m (54 ft)
   * Wingspan: 11.3 m (37 ft 2 in)
   * Height: 6.0 m (15 ft 6 in)
   * Wing area: 45.5 m² (490 ft²)
   * Empty weight: 8000~9,730 kg (21,460 lb)
   * Useful load: 5,500 kg (9 920 lb)
   * Max takeoff weight: 19,277 kg (42,498 lb)
   * Powerplant: 1× Saturn-Lyulka AL-31FN or Woshan WS-10A "Taihang" turbofan
         o Dry thrust: 89.43 kN / 89.17 kN (17,860 lbf / 20,052 lbf)
         o Thrust with afterburner: 122.5 kN / 129.4 kN (27,557 lbf / 29,101 lbf)

Performance

   * Maximum speed: Mach 2.0 at altitude
   * g-Limits: +9/-3 g (+88/-29 m/s², +290/-97 ft/s²
   * Combat radius: 750+ km[5] (1000 nm,
         o Maximum range: 2,940 km (1,370 nm,)
   * Service ceiling: 20,000 m (65,617 ft)
   * Wing loading: 335 kg/m² (64 lb/ft²)
   * Minimum thrust/weight:
         o With afterburner: 0.89

Armament

   * Guns: 2× 23 mm internal cannon
   * Normal Weapons load: 5,500 kg (9 920 lb)
   * Hardpoints: 11, 3 under each wing and 5 under the fuselage

Status: Avalible Cost: $47 Million

Air Superiority and Light Ground Attack Fighter ASLGAF or Typhoon F-2 (Real Life Typhoon F2)

Typhoon F2

General characteristics

   * Crew: 1(F-2) or 2(T-2)
   * Length: 15.96 m (52 ft 5 in)
   * Wingspan: 10.95 m (35 ft 11 in)
   * Height: 5.28 m (17 ft 4 in)
   * Wing area: 50 m² (540 ft²)
   * Empty weight: 11 000 kg (24,250 lb)
   * Loaded weight: 15 550 kg (34,280 lb)
   * Max takeoff weight: 23 500 kg (51,809 lb)
   * Powerplant: 2× Eurojet EJ200 afterburning turbofans, 60 kN dry; 90 kN with afterburner (13,500 lbf; 20,250 lbf) each

Performance

   * Maximum speed: Mach 2.25, 2390 km/h at high altitude; Mach 1.2, 1470 km/h at sea level; (1,480 mph; 915 mph) supercruise Mach 1.3+ at altitude with typical air-to-air armament
   * Range: 1390 km (864 mi)
   * Ferry range: 3790 km (2,300 mi)
   * Service ceiling: 19 812 m (65,000 ft [43])
   * Rate of climb: >315 m/s [44] (62,007 ft/min)
   * Wing loading: 311 kg/m² (63.7 lb/ft²)
   * Thrust/weight: 1.18

Armament

   * Gun: 1x 27 mm Mauser BK-27 cannon
   * Hard Points: Two wing edge and Four conformal Fuselage for AAM's. 3 Under each wing and 1 Large multiuse under Fuselage for Air to Ground weapons and AAM's

Status: Avalible Cost: $57 Million

Air Superiority and Strike Multirole Aircraft ASSMA or Super Wave FGR-1 (Real life based on Super 10 or J-10C project but stats similar to SU-37)

Super WaveSuper Wave Rear

General characteristics

   * Crew: Two (Pilot and Weapon Systems operator/Navigator)
   * Length: 22.2 m (72 ft 9 in)
   * Wingspan: 14.8 m (48 ft 3 in)
   * Height: 6.5 m (21 ft 1 in)
   * Wing area: 62.5 m² (667 ft²)
   * Empty weight: 18,500 kg (40,790 lb)
   * Max takeoff weight: 35,000 kg (77,160 lb)
   * Powerplant: 2× Saturn AL-31FN turbofans, 145 kN (32,000 lbf) each

Performance

   * Maximum speed: 2,500 km/h at high altitude (1,550 mph [1])
   * Range: 3,700 km (2,230 mi)
   * Service ceiling: 28,000 m (59,100 ft)

Armament

   * Guns: 1× 30mm internal cannon
   * Hardpoints: 2 Wing tip and 2 outboard underwing for AAM's. 3 under each wing and 3 under fuselage for air to ground weapons and AAM's

Status: Under Development Cost: Estimated $60 Million

Aircraft Update Programme

Super Phantom FGR-3AUP (Modernised Phantom)

In this project several new techniques have been used to turn the old phantoms into a 4th generation standard multirole fighter. The two seat cockpit is removed and replaced by a single cockpit with a bubble canopy and the space the second seat used to take up is now used by a 23mm cannon and extra fuel. Inside the new cockpit there is a state of the art array of LCD display and it is very simalar to the cockpit out of a F-35 fighter. The upgrade also includes the entire plane being controled by a "fly by wire" computer or allow more manuverblity. Thye engine have also been replaced by two Eurojet EJ200 afterburning turbofans to increase the fuel efficency of the fighter.

General characteristics

   * Crew: 1
   * Length: 63 ft 0 in (19.2 m)
   * Wingspan: 38 ft 4.5 in (11.7 m)
   * Height: 16 ft 6 in (5.0 m)
   * Wing area: 530.0 ft² (49.2 m²)
   * Airfoil: NACA 0006.4-64 root, NACA 0003-64 tip
   * Empty weight: 30,328 lb (13,757 kg)
   * Loaded weight: 41,500 lb (18,825 kg)
   * Max takeoff weight: 61,795 lb (28,030 kg)
   * Powerplant: 2× Eurojet EJ200 afterburning turbofans, 60 kN dry; 90 kN with afterburner (13,500 lbf; 20,250 lbf) each
   * Zero-lift drag coefficient: 0.0224
   * Drag area: 11.87 ft² (1.10 m²)
   * Aspect ratio: 2.77
   * Fuel capacity: 2,134 US gal internal
   * Maximum landing weight: 41,000 lb (16,706 kg)

Performance

   * Maximum speed: Mach 2.23 (1,472 mph, 2,370 km/h) at 40,000 ft (12,190 m)
   * Cruise speed: 752mph
   * Combat radius: 567 nm 
   * Ferry range: 2,203 nm with external fuel tanks
   * Service ceiling: 60,000 ft (18,300 m)
   * Rate of climb: 41,300 ft/min (210 m/s)
   * Wing loading: 78 lb/ft² (383 kg/m²)
   * Thrust/weight: 0.86
   * Lift-to-drag ratio: 8.58
   * Takeoff roll: 4,490 ft (1,370 m) at 53,814 lb (24,410 kg)
   * Landing roll: 3,680 ft (1,120 m) at 36,831 lb (16,706 kg)

Armament

   * Guns: 1× 23mm internal cannon
   * Weapons: 18,000Ib of missiles and bombs on 9 external hardpoints.