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Leopard 2 versus F/A-18E/F Super Hornet
Picture Author: Bundeswehr-Fotos

Wikimedia Source: [LINK]

Main Source: Flickr
Picture Author: ken H from Yokohama, Kanagawa-ken, Japan

Wikimedia Source: Wikimedia Commons

Main Source: Flickr: Mace 200 CAG bird on final for R/W19
Main battle tank Type Carrier-based multirole fighter
West Germany Place of Origin United States of America
1979–present Service Period and Status 2001 (IOC) - present (in service)
Krauss-Maffei Designer McDonnell Douglas
1970s Designed Period
Unit cost
2A6: US$5.74 million (2007)
Program & Unit Cost Program cost:
US$48.09 billion (through FY2011) - Total procurement

Unit cost:
US$70.5 million (2017 flyaway cost)
1979–present Production Period 1995–present
>3,200 Number Built 600 as of October 2018
Variants Boeing EA-18G Growler
Related Projects McDonnell Douglas F/A-18 Hornet
Empty weight:
2A6M: 60.2 t
2A6: 57.6 t
2A5: 57.3 t
2A4: 52 t

Combat weight:
2A6M: 62.5 t
2A6: 59.9 t - 61.7 t
2A5: 59.5 t
2A4: 55.15 t
Mass / Weight / Displacement Empty weight:
32,081 lb / 14,552 kg

Loaded weight:
47,000 lb / 21,320 kg (in air-to-air configuration)

Max. takeoff weight:
66,000 lb / 29,937 kg
2A6/2A6M: 10.97 m / 393 inches (gun forward) 2A4/2A5: 9.67 m Length 60 ft 1¼ in / 18.31 m
2A5/2A6/2A6M: 3.76 m / 148 in
2A4: 3.7 m
Width / Beam
2A5/2A6/2A6M: 3.030 m / 120 in
2A4: 2.79 m
Height 16 ft / 4.88 m
540 mm / 54 cm / 0.54 m Ground Clearance
4 Crew F/A-18E: 1 (pilot)
F/A-18F: 2 (pilot and weapon systems officer)
Wingspan 44 ft 8½ in / 13.62 m
Wing Area 500 ft² / 46.5 m²
Wing Loading 94.0 lb/ft² / 459 kg/m²
Powerplant 2 × General Electric F414-GE-400 turbofans
Thrust Dry thrust:
13,000 lbf / 62.3 kN each

Thrust with afterburner:
22,000 lbf / 97.9 kN each
1,200 litres / 264 imperial gallons / 317 US gallons Fuel Capacity Internal:
F/A-18E: 14,700 lb / 6,667 kg
F/A-18F: 13,760 lb / 6,241 kg

External:
Up to 4 × 480 gal tanks, totaling 13,040 lb / 5,914 kg
Road: ca. 340 l/100 km, ca. 340 km
Terrain: ca. 530 l/100 km, ca. 220 km
Average: ca. 410 l/100 km, ca. 280 km
Static test: 12.5 l/h, 72–93 hours (with 900–1,160 liters capacity)
Fuel Consumption
68 km/h / 42 mph 31 km/h backwards Speed At high altitude (40,000 ft / 12,190 m):
Mach 1.8 / 1,190 mph / 1,915 km/h
550 km / 340 mi (internal fuel) Operational Range Range:
1,275 nmi / 2,346 km clean plus two AIM-9s

Combat radius:
390 nmi / 449 mi / 722 km for interdiction mission

Ferry range:
1,800 nmi / 2,070 mi / 3,330 km
Service Ceiling 50,000+ ft / 15,000+ m
Rate of Climb 44,882 ft/min / 228 m/s
Thrust-to-Weight Ratio 0.93 (1.1 with loaded weight & 50% internal fuel)
24.1 PS/t / 17.7 kW/t Power-to-Weight Ratio
G-load Factor 7.6 g
Main armament:
2A6/2A6M:
1 × 120 mm Rheinmetall L/55 smoothbore gun (42 rounds)
2A4/2A5:
1 × 120 mm Rheinmetall L/44 smoothbore gun

Secondary armament:
2 × 7.62 mm MG3A1 (4,750 rounds)
Armament
2A5/2A6/2A6M: 21 t
2A4: 16 t
Turret Weight
2A6: 3rd generation composite; including high-hardness steel, tungsten and plastic filler with ceramic component Armor
MTU MB 873 Ka-501 liquid-cooled V12 twin-turbo diesel engine
1,500 PS / 1,479 hp / 1,103 kW at 2,600 rpm
Engine
Renk HSWL 354 Transmission
Torsion bar suspension Suspension
10 seconds Vehicle Rotation Time (360 degrees)
2A5/2A6/2A6M: 360° in 9 seconds (electric) Turret Rotation Time (360 degrees)
1,100 mm / 1.1 m Vertical Obstacle
3,000 mm / 3 m Trench Crossing
1,200 mm / 1.2 m without preparation
4,000 mm / 4 m with snorkel
Fording Depth
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