Pomilio Gamma
| Pomilio Gamma | |
|---|---|
| |
| The first Gamma prototype | |
| Role | Fighter |
| National origin | Italy |
| Manufacturer | Pomilio |
| First flight | 1918 |
| Primary user | Italy |
| Number built | 2 |
The Pomilio Gamma was an Italian fighter prototype of 1918.
Design and development
[edit]Gamma
[edit]The Pomilio company of Turin designed and manufactured the Gamma, a wooden, single-seat, single-bay biplane with wings of unequal span, the upper wing being of greater span than the lower. It was powered by a 149-kilowatt (200-horsepower) SPA 6A water-cooled engine driving a two-bladed tractor propeller. It had fixed, tailskid landing gear.[1]
The Gamma prototype first flew early in 1918. An Italian official commission observed a demonstration of it, and concluded that although it was fast and had good maneuverability, its rate of climb was insufficient to merit a production order.[2]
Gamma IF
[edit]Pomilio responded to the Gamma's shortcomings by building a second prototype, the Gamma IF, fitted with a more powerful Isotta Fraschini V.6 engine rated at 186 kilowatts (250 horsepower). An official commission saw a demonstration of the Gamma IF in 1918, but at first could not agree on whether it merited a production order. During the final weeks of World War I, the commission finally decided to order a small number of Gamma IF fighters, although the Gamma IF never entered active service.[3]
Variants
[edit]- Gamma
- First prototype with SPA 6A engine
- Gamma IF
- Second prototype with Isotta Fraschini engine
Operators
[edit]
Specifications (Gamma IF)
[edit]Data from Green, William, and Gordon Swanborough The Complete Book of Fighters: An Illustrated Encyclopedia of Every Fighter Aircraft Built and Flown, New York: SMITHMARK Publishers, 1994, ISBN 0-8317-3939-8
General characteristics
- Crew: 1
- Length: 6.30 m (20 ft 8 in)
- Wingspan: 7.99 m (26 ft 2.5 in)
- Wing area: 21.90 m2 (235.74 sq ft)
- Empty weight: 680 kg (1,499 lb)
- Gross weight: 950 kg (2,094 lb)
- Powerplant: 1 × Isotta Fraschini V.6 piston engine , 186 kW (250 hp)
Performance
- Maximum speed: 225 km/h (140 mph, 120 kn)
- Endurance: 3 hours
Notes:
- Time to 3,000 m (9,842 ft): 7 min 30 sec
Notes
[edit]References
[edit]
- Green, William, and Gordon Swanborough. The Complete Book of Fighters: An Illustrated Encyclopedia of Every Fighter Aircraft Built and Flown. New York: SMITHMARK Publishers, 1994. ISBN 0-8317-3939-8.
