Difference between revisions of "ANA Projects"

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(Aircraft Update Programme)
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== Aircraft Update Programme ==
 
== Aircraft Update Programme ==
  
=== Super Phantom FGR-3AUP (Modernised Phantom)
+
=== 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 Thye engine have also been replaced by two Eurojet EJ200 afterburning turbofans to increase the fuel efficency of the fighter.
 
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 Thye engine have also been replaced by two Eurojet EJ200 afterburning turbofans to increase the fuel efficency of the fighter.
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General characteristics
 
General characteristics
  
     * Crew: 2
+
     * Crew: 1
 
     * Length: 63 ft 0 in (19.2 m)
 
     * Length: 63 ft 0 in (19.2 m)
 
     * Wingspan: 38 ft 4.5 in (11.7 m)
 
     * Wingspan: 38 ft 4.5 in (11.7 m)
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     * Takeoff roll: 4,490 ft (1,370 m) at 53,814 lb (24,410 kg)
 
     * 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)
 
     * Landing roll: 3,680 ft (1,120 m) at 36,831 lb (16,706 kg)
 
  
 
= ANA Ships =
 
= ANA Ships =
  
 
= ANA Ground Forces =
 
= ANA Ground Forces =

Revision as of 04:08, 17 July 2007

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× General Electric J79-GE-17A axial compressor turbojets, 17,845 lbf (79.6 kN) each
   * Zero-lift drag coefficient: 0.0224
   * Drag area: 11.87 ft² (1.10 m²)
   * Aspect ratio: 2.77
   * Fuel capacity: 1,994 US gal (7,549 L) internal, 3,335 US gal (12,627 L) with three external tanks
   * Maximum landing weight: 36,831 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: 506 knots (585 mph, 940 km/h)
   * Combat radius: 367 nm (422 mi, 680 km)
   * Ferry range: 1,403 nm (1,615 mi, 2,600 km) with 3 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)

ANA Ships

ANA Ground Forces