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| F15

F15 Eagle fighter jet


When F-15 Eagle entered service in 1976 and was presented as competition to Soviet Mig-23 and Mig-25 which existence was revealed by the US intelligence. Until this day F-15 is still considered as one of the most successful fighter airplane ever built, tested in many conflicts around the globe even in the Gulf war.
This twin-engine beast manufactured by Boeing will stay in service with US Air Force until 2025.
Through the years more than ten versions were created from single-seat to two-seat. But one of the standard versions most used in combat was F-15C which was powered by two 65.3kN dry and 105.7kN with afterburn Pratt & Whitney turbofans.
It could reach speeds over 2.5 Mach (2655km/h) with maximum initial rate of climb over 50.000ft/min. All the specifications mean nothing in compare to the fact, that no F-15 until this day has been shot down in a dogfight. This airplane is also famous from its endurance when damaged. There is a true story how a pilot landed F-15 perfectly even though it was missing a wing.
Currently it is being used in Israel, Japan, Saudi Arabia and USA. Japan is using the F-15E variation.
Although F-15 is mainly known as being a fighter but it can also carry the ASM-135 anti-satellite weapon,
acting as a first stage launcher.

f15 eagle fighter jet

General characteristics

* Crew: 1
* Length: 63 ft 9 in (19.43 m)
* Wingspan: 42 ft 10 in (13.05 m)
* Height: 18 ft 6 in (5.63 m)
* Wing area: 608 ft² (56.5 m²)
* Airfoil: NACA 64A006.6 root, NACA 64A203 tip
* Empty weight: 28,000 lb (12,700 kg)
* Loaded weight: 44,500 lb (20,200 kg)
* Max takeoff weight: 68,000 lb (30,845 kg)
* Powerplant: 2× Pratt & Whitney F100-100 or -220 afterburning turbofans
o Dry thrust: 17,450 lbf (77.62 kN) each
o Thrust with afterburner: 25,000 lbf for -220 (111.2 kN for -220) each


* Maximum speed:
o High altitude: Mach 2.5+ (1,650+ mph, 2,660+ km/h)
o Low altitude: Mach 1.2 (900 mph, 1,450 km/h)
* Combat radius: 1,061 nmi (1,222 mi, 1,967 km) for interdiction mission
* Ferry range: 3,450 mi (3,000 nmi, 5,550 km) with conformal fuel tanks and three external fuel tanks
* Service ceiling: 65,000 ft (20,000 m)
* Rate of climb: >50,000 ft/min (254 m/s)
* Wing loading: 73.1 lb/ft² (358 kg/m²)
* Thrust/weight: 1.12 (-220)


* Guns: 1× internally mounted 20 mm (0.787 in) M61A1 gatling gun, 940 rounds
* Hardpoints: four wing, four fuselage, two wing stations, centerline station, optional fuselage pylons with a capacity of 16,000 lb (7,300 kg)
* Missiles:
o AIM-7 Sparrow
o AIM-9 Sidewinders