CASA C-101

CASA C-101 Aviojet

PaysEspagne
RôleAvion d’entraînement à réaction avancé et avion d’attaque léger
Premier vol27 juin 1977
Construit166

Lla CASA C-101 Aviojet est un avion d’entraînement avancé et d’attaque léger monomoteur à aile basse conçu et fabriqué par la société aéronautique espagnole Construcciones Aeronáuticas SA (CASA).

Source: CASA C-101 Aviojet sur Wikipedia

CASA C-101 Aviojet
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Voir aussi :

Seconde Guerre mondiale : l’histoire visuelle définitive de la Blitzkrieg à la bombe atomique (DK Definitive Visual Histories) - Amazon Carte par carte de la Seconde Guerre mondiale (carte par carte de l’histoire du Danemark) - Amazon


General Characteristics (Typical Trainer/Attack Variant)

The CASA C-101 Aviojet is a Spanish-designed low-wing, single-engine jet-powered aircraft developed for the dual role of advanced pilot training and light ground attack. It is configured with a tandem cockpit, where the instructor sits higher than the student to ensure excellent forward visibility. The aircraft is noted for its high fuel economy and long endurance for a jet trainer.

Property Typical Value (C-101BB/CC)
Rôle Advanced Jet Trainer / Light Attack
Fabricant CASA (Construcciones Aeronáuticas SA, Spain)
First Flight June 27, 1977
Crew 2 (Student and Instructor, in stepped tandem)
Length 12.50 m (41 ft 0 in)
Envergure 10.60 m (34 ft 9 in)
Max Takeoff Weight 6,300 kg (13,889 lb)

Design and Powerplant

  • Engine: One Honeywell TFE731-5-1J turbofan engine (C-101CC variant). Earlier variants used the TFE731-2 or TFE731-3.
  • Thrust Output: Approximately 19.13 kN (4,300 lbf) (military power reserve up to 20.91 kN / 4,700 lbf).
  • Design Feature: Features an unconventional, large internal weapons bay located beneath the rear cockpit, allowing for greater armament flexibility or the carriage of reconnaissance/ECM equipment.
  • Ejection Seats: Equipped with two Martin-Baker Mk10 zero/zero ejection seats.
  • Avionics: Later versions include a Head-Up Display (HUD) and mission computers supporting continuously computed attack modes (CCIP, CT, CCIL).
  • Aerobatic Team: The Spanish Air Forces Patrulla Águila aerobatic team uses a dedicated trainer version of the aircraft (C-101EB).

Performance and Armament

  • Maximum Speed: Up to 806 km/h (501 mph, 435 knots) at altitude (Mach 0.8 maximum dive speed).
  • Service Ceiling: 12,800 m (42,000 ft).
  • Ferry Range: 2,000 km (1,200 mi, 1,100 nmi).
  • Endurance: Maximum endurance up to 7 hours; typical training mission is 1 hour 10 minutes.
  • Rate of Climb: High rate, around 24.9 m/s (4,900 ft/min).
  • External Hardpoints: Six underwing hardpoints for external stores.
  • Maximum External Load: Up to 2,220 kg (4,894 lb).
  • Internal Armament Bay Options:
    • 30 mm DEFA cannon (with 130 rounds) OR
    • Twin 12.7 mm (0.50 in) M3 machine guns (with 440 rounds).
  • Typical Ordnance: Unguided rockets (70 mm FFAR), various general-purpose bombs, and AGM-65 Maverick air-to-ground missiles.

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