Specifications (F-8E)
Two AIM-9D Sidewinders mounted on the Y-pylons of the F-8 CrusaderData from The Great Book of Fighters and Quest for Performance Combat Aircraft since 1945
General characteristics
- Crew: 1
- Payload: 5,000 lb (2,300 kg) of weapons
- Length: 54 ft 3 in (16.53 m)
- Wingspan: 35 ft 8 in (10.87 m)
- Height: 15 ft 9 in (4.80 m)
- Wing area: 375 ft² (34.8 m²)
- Airfoil: NACA 65A006 mod root, NACA 65A005 mod tip
- Aspect ratio: 3.42:1
- Empty weight: 17,541 lb (7,956 kg)
- Loaded weight: 29,000 lb (13,000 kg)
- Powerplant: 1 × Pratt & Whitney J57-P-20A afterburning turbojet
- Dry thrust: 10,700 lbf (47.6 kN)
- Thrust with afterburner: 18,000 lbf (80.1 kN)
- Zero-lift drag coefficient: 0.0133
- Drag area: 5.0 ft² (0.46 m²)
- Fuel capacity: 1,325 US gal (5,020 L)
Performance
- Maximum speed: Mach 1.86 (1,225 mph, 1,975 km/h) at 36,000 ft (11,000 m)
- Cruise speed: 570 mph (495 knots (917 km/h))
- Combat radius: 450 mi (730 km)
- Ferry range: 1,735 mi (2,795 km) with external fuel
- Service ceiling: 58,000 ft (17,700 m)
- Rate of climb: 31,950 ft/min (162.3 m/s)
- Wing loading: 77.3 lb/ft² (377.6 kg/m²)
- Thrust/weight: 0.62
- Lift-to-drag ratio: 12.8
Armament
- Guns: 4× 20 mm (0.79 in) Colt Mk 12 cannons in lower fuselage, 125 rpg
- Hardpoints: 2× side fuselage mounted Y-pylons (for mounting AIM-9 Sidewinders and Zuni rockets) and 2× underwing pylon stations holding up to 4,000 lb (2,000 kg) of payload:
- Rockets:
- 2× LAU-10 rocket pods (each with 4× 5 inch (127mm) Zuni rockets)
- Missiles:
- Air-to-air missiles:
- 4× AIM-9 Sidewinder or Matra Magic (mounted only on F-8E(FN) of French Navy)
- Air-to-surface missiles:
- 2× AGM-12 Bullpup
- Air-to-air missiles:
- Bombs:
- 12× 250 lb (113 kg) Mark 81 bombs or
- 8× 500 lb (227 kg) Mark 82 bombs or
- 4× 1,000 lb (454 kg) Mark 83 bombs or
- 2× 2,000 lb (907 kg) Mark 84 bombs
Avionics
- Magnavox AN/APQ-84 or AN/APQ-94 Fire-control radar
Read more about this topic: Vought F-8 Crusader