IAI Kfir - Specifications (Kfir C.2)

Specifications (Kfir C.2)

Data from Jane's All The World's Aircraft 1982–83

General characteristics

  • Crew: One
  • Length: 15.65 m (51 ft 4¼ in)
  • Wingspan: 8.22 m (26 ft 11½ in)
  • Height: 4.55 m (14 ft 11¼ in)
  • Wing area: 34.8 m² (374.6 sq ft)
  • Empty weight: 7,285 kg (16,060 lb)
  • Loaded weight: 11,603 kg (25,580 lb) two 500 L drop tanks, two AAMs
  • Max. takeoff weight: 16,200 kg (35,715 lb)
  • Powerplant: 1 × IAl Bedek-built General Electric J-79-J1E turbojet
    • Dry thrust: 52.9 kN (11,890 lb st)
    • Thrust with afterburner: 79.62 kN (17,900 lb st)

Performance

  • Maximum speed: 2,440 km/h (1,317 knots, 1,516 mph) above 11,000 m (36,000 ft)
  • Combat radius: 768 km (415 nmi, 477 mi) (ground attack, hi-lo-hi profile, seven 500 lb bombs, two AAMs, two 1,300 L drop tanks)
  • Service ceiling: 17,680 m (58,000 ft)
  • Rate of climb: 233 m/s (45,950 ft/min)

Armament

  • Guns: 2× Rafael-built 30 mm (1.18 in) DEFA 553 cannons, 140 rounds/gun
  • Rockets: assortment of unguided air-to-ground rockets including the Matra JL-100 drop tank/rocket pack, each with 19× SNEB 68 mm rockets and 66 US gallons (250 liters) of fuel
  • Missiles: 2× AIM-9 Sidewinders or Shafrir or Python-series AAMs; 2× Shrike ARMs; 2× AGM-65 Maverick ASMs
  • Bombs: 5,775 kg (12,730 lb) of payload on nine external hardpoints, including bombs such as the Mark 80 series, Paveway series of LGBs, Griffin LGBs, TAL-1 OR TAL-2 CBUs, BLU-107 Matra Durandal, reconnaissance pods or Drop tanks

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