Aeritalia G.91
The
Aeritalia G.91, also known as the
Fiat G.91 and
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 thirty-five years.
In
1953, European aircraft manufacturers were invited by NATO to submit aircraft for evaluation for the "LWSF" (Light Weight Strike Fighter) role. The aircraft first flew on
August 1 1956 and the competing designs were evaluated in
1957. Besides the G.91, these included the
Northrop N156,
Dassault Étendard IV,
Sud-Est Baroudeur,
Aerfer Ariete and
Breguet Taon. Despite the G.91's impressive performance in trials, the
French government preferred to pursue development of the locally-designed Étendard, and the
British government 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 would later go on to serve for many years with the Italian
aerobatic team, the
Frecce Tricolori).
The first G.91s entered service in
1958. Aeritalia built 174 G.91s for Italy, plus 144 for Germany (including 50 that had been ordered and then cancelled by
Greece and
Turkey). Another 294 were built in Germany by
Flugzeug-Union Süd (a consortium of former competitors
Messerschmitt,
Heinkel, and
Dornier). These were the first jet combat aircraft built in Germany since the
Second World War. 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.
From
1961,
Portugal began to purchase the G.91 to deploy to her former 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F-86 Sabres, which were withdrawn following US protests over the use of these aircraft that had originally been supplied for defensive purposes. Portuguese G.91s continued in this role until the withdrawal from Africa in
1975.
Portugal finally phased out the last of her G.91s in
1993, and Italy in
1995. There are numerous examples preserved in museums around the world.
* Germany
* Italy
* Portugal
* Angola
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.91PAN -
* G.91R/1 -
* G.91R/1A -
* G.91R/1B -
* G.91R/3 - Orpheus engine; 2 DEFA cannons
* G.91R/4 - Orpheus engine; 4 Colt-Browning cannons
* G.91T/1 -
* G.91T/3 -
* G.91T/4 -
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 in
1966 and displayed a vast improvement in speed, range, payload, and maneuverability. It increased maximum speed to 600 kt (1,110 km/h, 690 mph,
Mach 0.91). The machine guns were replaced by a pair of
DEFA 552 30mm cannon with 125 rounds per gun.
|
Orthographically projected diagram of the Aeritalia G-91Y. |
{{aircraft specifications
plane or copter?=plane | jet or prop?=jet
| crew=1 | length main=10.3 m | length alt=33 ft 9 in | span main=8.56 m | span alt=28 ft 1 in | height main=4.0 m | height alt=13 ft 1 in | area main=16.4 m² | area alt=177 ft² | empty weight main=3,100 kg | empty weight alt=6,830 lb | loaded weight main=5,440 kg | loaded weight alt=11,990 lb | max takeoff weight main=5,500 kg | engine (jet)=Bristol-Siddeley Orpheus 803 | type of jet=turbojet | number of jets=1 | thrust main=22.2 kN | max speed main=1,075 km/h | max speed alt=580 knots, 668 mph | range main=1,150 km | range alt=621 nm, 715 miles | ceiling main=13,100 m | ceiling alt=43,000 ft | climb rate main=30 m/s | climb rate alt=6,000 ft/min | loading main=331 kg/m² | loading alt=67.8 lb/ft² | guns=4× 12.7 mm (0.50 in) 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){{aircontent | related= | similar aircraft= * F-5 Freedom Fighter * Folland Gnat *Lim-6 | sequence= | see also= | lists=*Photos of G.91R-3 at Wolfgang Bredow page
|