(Fiat) G.91 @·AIRCRAFTUBE

  • Fiat G.91PAN Frecce Tricolori Fiat G.91PAN Frecce Tricolori
    Fiat G.91PAN Frecce Tricolori
  • Fiat G.91PAN Frecce Tricolori Fiat G.91PAN Frecce Tricolori
    Fiat G.91PAN Frecce Tricolori
  • Fiat G.91PAN Frecce Tricolori Fiat G.91PAN Frecce Tricolori
    Fiat G.91PAN Frecce Tricolori
  • Fiat G.91 R1 Fiat G.91 R1
    Fiat G.91 R1
  • Fiat G.91R Fiat G.91R
    Fiat G.91R
  • Fiat G.91T - 60 Stormo Fiat G.91T - 60 Stormo
    Fiat G.91T - 60 Stormo
  • Fiat G-91 - Luftwaffe Museum Fiat G-91 - Luftwaffe Museum
    Fiat G-91 - Luftwaffe Museum
  • Fiat G-91 Fiat G-91
    Fiat G-91
  • Fiat G.91 Fiat G.91
    Fiat G.91

Fiat G.91

The Fiat G.91, nicknamed "Gina", was an Italian fighter aircraft that was intended to serve as standard equipment for NATO air forces in the 1960s. It was eventually only adopted by three - the Italian Air Force, West Germany's Luftwaffe, and the Portuguese Air Force - but enjoyed a long service life that extended over 35 years. It was widely used by Portugal in the Portuguese Colonial War in Africa.

In 1953, European aircraft manufacturers were invited by NATO to submit aircraft for evaluation for the Light Weight Strike Fighter (LWSF) role. The G.91 was designed to this specification by the Italian engineer Giuseppe Gabrielli, hence the "G" designation. The competition was intended to produce an aircraft that was light, small, expendable, equipped with basic weapons and avionics and capable of operating with minimal ground support. These specifications were developed for two reasons: the first was the nuclear threat to large air bases, many cheaper aircraft could be better dispersed, and the other was to counter the trend towards larger and more expensive aircraft.

The technical requirements were:

1,100 m takeoff distance over a 15 m obstacle.
Capability to operate from grass strips and streets.
Max. speed of 0.95 Mach.
Range of 280 km with 10 min over the target.
Armoured protection for the pilot and the fuel tanks.
Four 12.7 mm or two 20 mm or 30 mm guns.
A maximum of 2,200 kg empty weight and 4,700 kg maximum weight.

The designs were required within two months of the competition.

Fiat Aviazione proposed the G.91 and other companies entered ten projects. These were assessed starting on 18 March 1953 by AGARD (Advisory Group for Aeronautical Research and Development) under the leadership of Von Karman. The challenge of providing an engine that matched the requirements of lightness and power, reliability and ease of maintenance was solved by using the Bristol Orpheus turbojet.

The G.91 first flew on 9 August 1956 and the competing designs were evaluated in 1957. Besides the G.91, these included the Northrop N-156, Dassault Étendard IV, Sud-Est Baroudeur, Aerfer Ariete and Breguet Taon. Despite the G.91's impressive performance in trials, which resulted in its selection as the winner of the contest, after the loss of the Fiat G.91 prototype, the French government preferred to pursue development of the locally-designed Étendard. The British government similarly ignored the competition to concentrate on Hawker Hunter production for the same role. In fairness, it should also be pointed out that the Italian government also ordered the G.91 for the Italian Air Force before the results of the competition were known. These pre-production machines (G.91 PAN) would later go on to serve for many years with the Italian aerobatic team, the Frecce Tricolori. The type was also considered by Austria, Norway, Switzerland, and even the United States Army, which briefly evaluated the type as a possible Forward Air Control (FAC) aircraft before relinquishing all fixed-wing aircraft operations to the USAF.

The re-engineering work on G.91 was very extensive and resulted in the second prototype being fitted with a bigger tail, 6 cm higher canopy, a ventral fin and some other modifications. It flew in July 1957, but it was not sent to the final evaluation. The third and fourth G.91 prototypes were sent to France, for the competition. The later G.91R was 20% heavier than estimated, but it was powered by a Bristol Orpheus 801 to compensate. It was capable of supersonic speed in a dive, as demonstrated by test pilot Riccardo Bignamini on 20 February 1957 when he broke the sound barrier four times in 9,000 m dives.

Aeritalia built 174 G.91s for Italy, plus 144 R/3 variants for West Germany (including 50 that had been ordered and then cancelled by Greece and Turkey). The German order involved a production run of 294 G.91s built in Germany by Flugzeug-Union Süd (a consortium of former competitors Messerschmitt, Heinkel and Dornier). These were the first combat aircraft built in Germany since World War II. The first order was for 50 machines from Aeritalia, then Dornier and other German firms had an order for 232 machines, later increased to 294. The Luftwaffe also bought 44 G-91T/3 two-seat trainers and another 22 were produced in Germany, ending production in 1972.

The Luftwaffe had intended to equip a further four wings with the G.91R/3 but initial operating experience with the type left the Luftwaffe disappointed with the aircraft's performance and further orders were cut. Some Luftwaffe G.91s were emblazoned with "pig" emblems as a comment on the aircraft's lacklustre performance.

Operational history

The first G.91s entered service in August 1958, with 103 Gruppo, 5 Aerobrigata, called "Caccia Tattici Leggeri (CTL)", based at Pratica di Mare, the same with Reparto Sperimentale di Volo. The next operational unit was 14 Gruppo, Seconda Aerobrigata in 1961. This unit had its role shifted to tactical support, because her groups were 14, 103 (dispatched from 5 A-B to this Aerobrigade) and 13 (only in reserve). All them were based at Treviso-Sant'Angelo.

The differences in firepower (two 30 mm DEFA guns, four underwing pylons) and improved avionics made the German machines far more effective than Italian examples, even if they were heavier. In addition, mass-production made the G.91 force more credible. The first examples, 12 Fiat-Aeritalias built aircraft, were delivered to Aufklarungsgeschwader (AG)53 for training and experiments. This unit was based at Erding, near Munich along with Waffenschule 50. On 20 July 1960 the first Dornier was tested.

From 1965, Portugal began to purchase the G.91 to deploy to its African colonies of Mozambique, Guinea-Bissau and Angola in the close-support role. The first 40 were purchased second-hand from the Luftwaffe, out of the aircraft that had originally been produced for Greece and which differed from the rest of the Luftwaffe G.91s sufficiently to create maintenance problems. The aircraft replaced the F-86 Sabre. Portuguese G.91s continued in this role until the withdrawal from Africa in 1975. Portugal finally phased out the last of its G.91s in 1993, and Italy in 1995.

Variants

Trainer and reconnaissance variants were produced right from the start of G.91 production, but the basic design of the aircraft remained virtually unchanged throughout almost the entire production run of the aircraft. The one major difference is that the R series aircraft were single seaters, while the T series aircraft had two seats. To accommodate the extra seat, the T series aircraft had a slightly longer fuselage.

G.91 - Prototypes and pre-production aircraft.
G.91R/1 - Light attack-reconnaissance aircraft, fitted with modified nose housing three cameras.
G.91R/1A - Revised instrumentation.
G.91R/1B - Strengthened airframe.
G.91R/3 - Single-seat ground-attack, reconnaissance version for the Luftwaffe. Powered by a Rolls-Royce Orpheus turbojet engine. Armed with two 30 mm DEFA cannons.
G.91R/4 - Similar to the G.91R/3, but armed with four .50-inch (or 12.7 mm) Colt-Browning machine-guns. Powered by a Rolls-Royce Orpheus turbojet engine.
G.91T/1 - Trainer version of G.91R/1 for Italian Air Force.
G.91T/3 - Trainer version for Luftwaffe.
G.91PAN - Aerobatic display aircraft for Frecce Tricolori, converted from pre-production G.91s.
G.91Y: An additional 67 aircraft built by Aeritalia were significantly uprated from earlier versions. These aircraft, designated G.91Y replaced the original Bristol-Siddeley Orpheus engine with two General Electric J85 units.The G.91Y first flew on 12 December 1966 and displayed a vast improvement in speed, range, payload, and maneuverability. It increased maximum speed to 600 kt (or 1,110 km/h, or 690 mph, or Mach 0.91). The machine guns were replaced by a pair of DEFA 552 30mm cannons with 125 rounds per gun. All the aircraft built served with the Italian Air Force.

Operators

German Luftwaffe.
Italian Air Force.
Portuguese Air Force (1966-1993).

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This text is available under the Creative Commons Attribution-ShareAlike License
Source : Article Fiat G.91 of Wikipedia ( authors )

Specifications (G.91R)

  • Crew : One pilot.
  • Length : 10.3 m (or 33 ft 9 in).
  • Height : 4 m (or 13 ft 1 in).
  • Wingspan : 8.56 m (or 28 ft 1 in).
  • Wing area : 16.4 m² (or 177 ft²).
  • Wing loading : 331 kg/m² (or 67.8 lb/ft²).
  • Empty weight : 3,100 kg (or 6,830 lb).
  • Loaded weight : 5,440 kg (or 11,990 lb).
  • Max. takeoff weight : 5,500 kg (or 12,100 lb).
  • Max. speed : 1,075 km/h (or 580 knots, or 668 mph).
  • Range : 1,150 km (or 621 Nm, or 715 miles).
  • Service ceiling 13,100 m (or 43,000 ft).
  • Rate of climb : 30 m/s (or 6,000 ft/min).
  • Powerplant : One Bristol-Siddeley Orpheus 803 turbojet.
  • Thrust : 22.2 kN (or 5,000 lbf).
  • Thrust/weight : 0.42.
  • Armament : Four 12.7 mm (or 0.50 in) M2 Browning machine guns, 500 kg (1,100 lb) of bombs, rockets, fuel tanks or gunpods on four underwing hardpoints (R/1), 680 kg (R/3, R/4), 1814 kg (Y).

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This text is available under the Creative Commons Attribution-ShareAlike License
Source : Article Fiat G.91 of Wikipedia ( authors )
Fiat G.91 : Your comments on this subject
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