Aircraft Design Project for fighter aircraft

Fighter aircraft General characteristics: Crew

:

1

Length

:

17.8m

Wingspan

:

11.74m

Height

:

5.09m

Wing area

:

55.93m²

Empty weight

:

14625kg(143422.26N)

Loaded weight

:

23124kg(226768.97N)

Maximum Take-off weight

:

30625kg(300328.66N)

Dry Thrust

:

86212.5N

Thrust with After Burner

:

131625N

Fuel Capacity

:

9220.5kg(90422.22N)

Maximum speed

:

1.86Mach(1380miles/hour or 2221km/hour)

Range

:

3551km(2207miles or 1917 Nm)

Service Celing

:

18025m(59137ft)

Rate of climb

:

350m/s

Wing Loading

:

450-550kg/m²(4400-5400N/m²)

Thrust/Weight

:

0.99

Maximum g-load

:

9g

Performance:

Armament: Guns: 1*20mm 20 mm (0.787 in) M61 Vulcan 6-barreled Gatling cannon, 511 rounds Hardpoints: 2× wing-tip Air-to-air missile launch rails, 6× under-wing & 3× under-fuselage pylon stations holding up to 17,000 lb (7,700 kg) of disposable stores Rockets: 4×LAU-61/LAU-68 rocket pods (each with 19× /7× Hydra 70 mm rockets, respectively) 4×LAU-5003 rocket pods (each with 19× CRV7 70 mm rockets) 4×LAU-10 rocket pods (each with 4× Zuni 127 mm rockets) Missiles: Air-to-air missiles: 2× AIM-7 Sparrow 6× AIM-9 Sidewinder 6× AIM-120 AMRAAM 6× IRIS-T 6× Python-4 

Air-to-ground missiles: 6× AGM-65 Maverick 4× AGM-88 HARM AGM-158 Joint Air-to-Surface Standoff Missile (JASSM)



Anti-ship missiles: 2× AGM-84 Harpoon

Avionics AN/APG-68 radar MIL-STD-1553 bus