Fiat G-91R3

Fiat G.91

ZemljaItalia
UloguBorac-bombarder
Prvi let9 Avgust 1956
Izgradio770

Čaj Fiat G.91 je italijanski mlazni borbeni avion koji je projektovao i napravio Fijat Aviazione, a koji se kasnije spojio u Aeritaliju. G.91 ima svoje poreklo na takmičenju NBMR-1 koje je organizovao NATO 1953. Nakon što je pregledao više podnesaka, G.91 je izabran kao pobednički dizajn takmičenja NBMR-1.

Izvor: Fiat G.91 na Vikipediji
Fiat G-91R3 Walk Around
PhotographerUlrich Wrede
LocalisationUnknow
Photos53
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FotografTiberio Riva
LokalizacijaNepoznato
Fotografije193

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Fiat G.91 Reference Walk Around
FotografPhilippe Agulhon
LokalizacijaNepoznato
Fotografije23
Fiat G91 R3 Walk Around
FotografJose Brito
LokalizacijaNepoznato
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Fiat G91 T1 Walk Around
FotografUnknow
LokalizacijaNepoznato
Fotografije18

General Characteristics and Role

The Fiat G.91 was a lightweight, low-cost jet fighter designed in Italy to fulfill a NATO requirement for a “Light Weight Strike Fighter” (LWFS) in the 1950s. The G.91R/3 was the primary variant procured by the West German Air Force (Luftwaffe). The ‘R’ designation signifies its primary role in tactical reconnaissance, achieved by installing a camera nose section containing three Vinten cameras. The G.91R/3 also retained substantial ground attack capabilities, making it a versatile light fighter-bomber. It was rugged, simple to maintain, and capable of operating from rough forward airstrips, fitting the original NATO doctrine for decentralized combat operations. It became the backbone of the Luftwaffe’s light attack force for two decades.

Property Typical Value (G.91R/3)
Ulogu Tactical Reconnaissance, Light Attack, Fighter-Bomber
National Origin Italy (License-built by Dornier/Focke-Wulf in Germany)
Proizvođača Fiat Aviazione (now Aeritalia), Dornier, Focke-Wulf
First Flight (G.91) 9 Avgust 1956
Posada 1 (Pilot)
Dužina 10.30 m (33 ft 9 in)
Raspon krila 8.56 m (28 ft 1 in)
Visina 4.00 m (13 ft 1 in)
Empty Weight 3,100 kg (6,834 lb)
Max Takeoff Weight 5,500 kg (12,125 lb)

Powerplant and Performance

  • Engine: 1 x Bristol Siddeley Orpheus Mk. 803 turbojet.
  • Thrust: 22.2 kN (5,000 lbf).
  • Maximum Speed: 1,075 km/h (668 mph; 580 kn) at sea level (Mach 0.86).
  • Range (Combat): 400 km (250 mi; 220 nmi).
  • Service Ceiling: 13,100 m (43,000 ft).

Armament and Reconnaissance

  • Fixed Armament: 4 x 30 mm DEFA cannons (G.91R/3 variant) or 4 x 12.7 mm Browning machine guns (other variants).
  • Hardpoints: 4 underwing hardpoints.
  • Maximum Payload: 1,000 kg (2,200 lb), including bombs, rockets, and external fuel tanks.
  • Reconnaissance: The G.91R/3 features three forward and side-facing Vinten cameras in the nose section for photographic tactical reconnaissance missions.
  • Service Life: The G.91 served in the Luftwaffe until 1982, when it was replaced by the Dassault/Dornier Alpha Jet.

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