substitutos:
Rafale:caraceteristicas:
Crew: 1–2
Length: 15.27 m (50.1 ft)
Wingspan: 10.80 m (35.4 ft)
Height: 5.34 m (17.4 ft)
Wing area: 45.7 m² (492 ft²)
Empty weight: 9,060 kg (20,000 lb)
Useful load: 9,500 kg (21,000 lb)
Max takeoff weight: 24,500 kg (54,000 lb)
Powerplant:
2× SNECMA M88-2 turbofans
Dry thrust: 50 kN (11,250 lbf) each
Thrust with afterburner: 75 kN (17,000 lbf) each
Performance:
Maximum speed: >Mach 1.8 (2,130 km/h, 1,320 mph)
Range: 1,800 km (970 nm, 1,100 mi)
Service ceiling: 18,000 m (60,000 ft)
Rate of climb: >305 m/s [8] (60,000 ft/min)
Wing loading: 326 kg/m² (83 1/3 lb/ft²)
Thrust/weight: 1.13
Armament:
Guns: 1× 30 mm (1.18 in) GIAT 30/719B cannon with 125 rounds
Air-to-air:
MICA IR/EM or
AIM-9 Sidewinder or
AIM-132 ASRAAM or
AIM-120 AMRAAM or
MBDA Meteor or
Magic II
Air-to-ground:
MBDA Apache or
SCALP EG or
AASM or
AM 39 Exocet or
ASMP nuclear missile
Avionics:
Thales RBE2 radar
Thales SPECTRA electronic warfare system.
Thales/SAGEM OSF (Optronique Secteur Frontal) infrared search and track system.
F35características:
Note: Some information is estimated.
General characteristics
Length: 50 ft 6 in (15.37 m)
Wingspan: 35 ft 0 in (10.65 m)
Height: 17 ft 4 in (5.28 m)
Wing area: 459.6 ft² (42.7 m²)
Empty weight: 26,000 lb (12,000 kg)
Loaded weight: 44,400 lb (20,100 kg)
Max takeoff weight: 60,000 lb (27,200 kg)
Powerplant:
1× Pratt & Whitney F135 afterburning turbofan
Dry thrust: 25,000 lbf (111 kN)
Thrust with afterburner: >40,000 lbf (178 kN)
Secondary Powerplant: 1× General Electric/Rolls-Royce F136 afterburning turbofan, >40,000 lbf (178 kN) [in development]
Lift fan (STOVL): 1× Rolls-Royce Lift System driven from either F135 or F136 power plant, 18,000 lbf (80 kN)
Performance
Maximum speed: Mach 1.6+ (1,200 mph, 1,931 km/h)
Range: A: 1,200 nmi; B: 900 nm; C: 1400 nm (A: 2,200 km; B: 1,667 km; C: 2,593 km) on internal fuel
Combat radius: 600 nmi (690 mi, 1,110 km)
Wing loading: 91.4 lb/ft² (446 kg/m²)
Thrust/weight:
With full fuel: A: 0.89; B: 0.92; C: 0.81
With 50% fuel: A: 1.12; B: 1.10; C: 1.01
G-Limits
F-35A: +9G
F-35B: +7G
F-35C: +7.5G
Armament
1 × GAU-12/U 25 mm cannon - slated to be mounted internally with 180 rounds in the F-35A and fitted as an external pod with 220 rounds in the F-35B and F-35C.
Internally (current planned weapons for integration), up to four AIM-120 AMRAAM, AIM-9X Sidewinder or AIM-132 ASRAAM internally or two air-to-air and two air-to-ground weapons (up to two 2,000 lb weapons in A and C models; two 1000 lb weapons in the B model) in the bomb bays.
These could be AMRAAM, the Joint Direct Attack Munition (JDAM) - up to 2,000 lb (910 kg), the Joint Standoff Weapon (JSOW), Small Diameter Bombs (SDB) - a maximum of four in each bay, the Brimstone anti-armor missiles, Cluster Munitions (WCMD) and High Speed Anti-Radiation Missiles (HARM). The MBDA Meteor air-to-air missile is currently being adapted to fit internally in the missile spots and may be integrated into the F-35.
Gripencaracterísticas:
Crew: 1-2
Dimensions:
Length: 14.1 m (46 ft 3 in)
Wingspan: 8.4 m (27 ft 7 in)
Height: 4.5 m (14 ft 9 in)
Wing area: 25.54 m (274.9 ft)
Weights:
Empty weight: 6,620 kg (14,600 lb)
Loaded weight: 8,720 kg (19,200 lb)
Maximum gross takeoff weight: 14,000 kg (31,000 lb)
Powerplant:
1× Volvo Aero RM12 (GE404) afterburning turbofan, 54 kN dry, 80 kN with afterburner (12,000 lbf / 18,000 lbf)
Performance:
Maximum speed: Mach 2
Range: 800 km (500 mi)
Service ceiling: 15,000 m (50,000 ft)
Thrust/weight: 0.63:1
Armament:
1x 27 mm Mauser BK-27 cannon
6x AIM-9 Sidewinder
4x AIM-120 AMRAAM; or MICA
AGM-65 Maverick, KEPD 150, or various other laser-guided bombs, rocket pods.
Eurofighter Typhoon:caracteristicas:
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 2.0+, 2390 km/h (1,480 mph) at high altitude; Mach 1.2, 1470 km/h (915 mph) at sea level; supercruise Mach 1.3+ at altitude with typical air-to-air armament
Range: 1390 km (864 mi)
Service ceiling: 18 000 m (60,000 ft)
Rate of climb: 255 m/s (50,000 ft/min)
Wing loading: 311 kg/m² (63.7 lb/ft²)
Thrust/weight: 1.18
Armament:
gun: 1x 27 mm Mauser BK-27 cannon
air-to-air missiles: AIM-9 Sidewinder, AIM-132 ASRAAM, AIM-120 AMRAAM, IRIS-T, MBDA Meteor
air-to-ground missiles: AGM-84 Harpoon, AGM-88 HARM, AGM Armiger, ALARMs, Storm Shadow (AKA "Scalp EG"), Brimstone, Taurus, Penguin
bombs: Paveway 2, Paveway 3, Enhanced Paveway, JDAM
Laser designator, e.g. LITENING pod
http://quicklink.all.googlepages.com/f16 block60características:
Engine: One General Electric F110-GE-132 turbofan, rated at 19,000 lb.s.t. dry and 32,500 lb.s.t. with afterburning.
Performance: Maximum short-endurance speed: Mach 2.02 (1333 mph) at 40,000 feet. Maximum sustained speed Mach 1.89 (1247 mph) at 40,000 feet.
Dimensions: wingspan 31 feet 0 inches, length 49 feet 4 inches, height 16 feet 8 1/2 inches, wing area 300 square feet.
Weights: around 22,000 pounds empty, 29,000 pounds normal loaded (air-to-air mission), 46,000 pounds maximum takeoff.
full armament capability of the Block 50's and adds several new capabilities. The Block 60's basic design and weapon interfaces are compatible with projected future weapons including new air-to-air missiles such as the AIM-132 Advanced Short Range Air-to-Air Missile (ASRAAM). The aircraft will also support all-weather standoff weapons, such as the AGM-154 Joint Standoff Weapon (JSOW), and AGM-84E Standoff Land Attack Missile (SLAM).
http://www.f-16.net/f-16_versions_article10.htmldepois destas caracteristicas todas já podemos começar a discutir a sério qual o melhor substituto, se faltar algum podem por.