Difference between revisions of "ANA Projects"
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* Loaded weight: 41,500 lb (18,825 kg) | * Loaded weight: 41,500 lb (18,825 kg) | ||
* Max takeoff weight: 61,795 lb (28,030 kg) | * Max takeoff weight: 61,795 lb (28,030 kg) | ||
− | * Powerplant: 2× | + | * 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 | * Zero-lift drag coefficient: 0.0224 | ||
* Drag area: 11.87 ft² (1.10 m²) | * Drag area: 11.87 ft² (1.10 m²) | ||
* Aspect ratio: 2.77 | * Aspect ratio: 2.77 | ||
− | * Fuel capacity: | + | * Fuel capacity: 2,134 US gal internal |
− | * Maximum landing weight: | + | * Maximum landing weight: 41,000 lb (16,706 kg) |
Performance | Performance | ||
* Maximum speed: Mach 2.23 (1,472 mph, 2,370 km/h) at 40,000 ft (12,190 m) | * Maximum speed: Mach 2.23 (1,472 mph, 2,370 km/h) at 40,000 ft (12,190 m) | ||
− | * Cruise speed: | + | * Cruise speed: 752mph |
− | * Combat radius: | + | * Combat radius: 567 nm |
− | * Ferry range: | + | * Ferry range: 2,203 nm with external fuel tanks |
* Service ceiling: 60,000 ft (18,300 m) | * Service ceiling: 60,000 ft (18,300 m) | ||
* Rate of climb: 41,300 ft/min (210 m/s) | * Rate of climb: 41,300 ft/min (210 m/s) | ||
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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) | ||
+ | |||
+ | Armament | ||
+ | |||
+ | * Guns: 1× 23mm internal cannon | ||
+ | * Weapons: 18,000Ib of missiles and bombs on 9 external hardpoints. | ||
= ANA Ships = | = ANA Ships = | ||
= ANA Ground Forces = | = ANA Ground Forces = |
Latest revision as of 05:17, 17 July 2007
Contents
- 1 ANA Aircraft
- 1.1 The ANA Modern Fighter Family
- 1.1.1 The Light Multirole Fighter LMF or Wave FG-1 (Real Life J-10)
- 1.1.2 Air Superiority and Light Ground Attack Fighter ASLGAF or Typhoon F-2 (Real Life Typhoon F2)
- 1.1.3 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)
- 1.2 Aircraft Update Programme
- 1.1 The ANA Modern Fighter Family
- 2 ANA Ships
- 3 ANA Ground Forces
ANA Aircraft
The ANA Modern Fighter Family
The Light Multirole Fighter LMF or Wave FG-1 (Real Life J-10)
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)
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)
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.