Difference between revisions of "ANA Projects"
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== The ANA Modern Fighter Family == | == The ANA Modern Fighter Family == | ||
− | = The Light Multirole Fighter LMF or Wave FG-1 (Real Life J-10) [[Image: | + | = The Light Multirole Fighter LMF or Wave FG-1 (Real Life J-10) [[Image:Chengdu_J-10_3-view.gif|right|300px|An orthogonally projected diagram of the Wave FG-1]] |
+ | General characteristics | ||
+ | * Crew: 1 (basic), 2 (trainer variant)[5] | ||
+ | * Length: 16.5 m (54 ft[citation needed]) | ||
+ | * Wingspan: 11.3 m (37 ft 2 in[citation needed]) | ||
+ | * Height: 6.0 m (15 ft 6 in[citation needed]) | ||
+ | * Wing area: 45.5 m² (490 ft²[citation needed]) | ||
+ | * Empty weight: 8000~9,730 kg (21,460 lb[13]) | ||
+ | * Useful load: 5,500 kg (9 920 lb[citation needed]) | ||
+ | * Max takeoff weight: 19,277 kg (42,498 lb[citation needed]) | ||
+ | * 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[5] | ||
+ | * g-Limits: +9/-3 g (+88/-29 m/s², +290/-97 ft/s²[citation needed] | ||
+ | * Combat radius: 750+ km[5] (1000 nm,[citation needed] | ||
+ | o Maximum range: 2,940 km (1,370 nm,[citation needed]) | ||
+ | * 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 | ||
+ | * Missiles: | ||
+ | o Air-to-air: PL-8, PL-9, PL-11, PL-12 | ||
+ | o Air-to-surface: PJ-9, YJ-9K, 90 mm unguided rocket launcher pods | ||
+ | * Bombs: laser-guided bombs (LT-2), glide bombs (LS-6) and unguided bombs | ||
Revision as of 03:01, 16 July 2007
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)[5] * Length: 16.5 m (54 ft[citation needed]) * Wingspan: 11.3 m (37 ft 2 in[citation needed]) * Height: 6.0 m (15 ft 6 in[citation needed]) * Wing area: 45.5 m² (490 ft²[citation needed]) * Empty weight: 8000~9,730 kg (21,460 lb[13]) * Useful load: 5,500 kg (9 920 lb[citation needed]) * Max takeoff weight: 19,277 kg (42,498 lb[citation needed]) * 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[5] * g-Limits: +9/-3 g (+88/-29 m/s², +290/-97 ft/s²[citation needed] * Combat radius: 750+ km[5] (1000 nm,[citation needed] o Maximum range: 2,940 km (1,370 nm,[citation needed]) * 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 * Missiles: o Air-to-air: PL-8, PL-9, PL-11, PL-12 o Air-to-surface: PJ-9, YJ-9K, 90 mm unguided rocket launcher pods * Bombs: laser-guided bombs (LT-2), glide bombs (LS-6) and unguided bombs