Difference between revisions of "ANA Projects"
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General characteristics | General characteristics | ||
| − | * Crew: 1 (basic), 2 (trainer variant) | + | * Crew: 1 (basic), 2 (trainer variant) |
| − | * Length: 16.5 m (54 ft | + | * Length: 16.5 m (54 ft) |
| − | * Wingspan: 11.3 m (37 ft 2 in | + | * Wingspan: 11.3 m (37 ft 2 in) |
| − | * Height: 6.0 m (15 ft 6 in | + | * Height: 6.0 m (15 ft 6 in) |
| − | * Wing area: 45.5 m² (490 ft² | + | * Wing area: 45.5 m² (490 ft²) |
| − | * Empty weight: 8000~9,730 kg (21,460 lb | + | * Empty weight: 8000~9,730 kg (21,460 lb) |
| − | * Useful load: 5,500 kg (9 920 lb | + | * Useful load: 5,500 kg (9 920 lb) |
| − | * Max takeoff weight: 19,277 kg (42,498 lb | + | * Max takeoff weight: 19,277 kg (42,498 lb) |
* Powerplant: 1× Saturn-Lyulka AL-31FN or Woshan WS-10A "Taihang" turbofan | * 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 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) | o Thrust with afterburner: 122.5 kN / 129.4 kN (27,557 lbf / 29,101 lbf) | ||
Performance | Performance | ||
| − | * Maximum speed: Mach 2.0 at altitude | + | * Maximum speed: Mach 2.0 at altitude |
| − | * g-Limits: +9/-3 g (+88/-29 m/s², +290/-97 ft/s² | + | * g-Limits: +9/-3 g (+88/-29 m/s², +290/-97 ft/s² |
| − | * Combat radius: 750+ km[5] (1000 nm, | + | * Combat radius: 750+ km[5] (1000 nm, |
| − | o Maximum range: 2,940 km (1,370 nm, | + | o Maximum range: 2,940 km (1,370 nm,) |
* Service ceiling: 20,000 m (65,617 ft) | * Service ceiling: 20,000 m (65,617 ft) | ||
* Wing loading: 335 kg/m² (64 lb/ft²) | * Wing loading: 335 kg/m² (64 lb/ft²) | ||
Revision as of 03:08, 16 July 2007
Contents
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 * Hardpoints: 11, 3 under each wing and 5 under the fuselage
