| PG-1 | |
|---|---|
| |
| Role | Pursuit and ground attack aircraft |
| National origin | United States |
| Manufacturer | Aeromarine |
| Design group | U.S. Army Engineering Division |
| First flight | 22 August 1922[1] |
| Number built | 3[1] |
The Aeromarine PG-1 was an American single-seat pursuit (fighter) and ground attack (PG) biplane developed by the Engineering Division of the United States Army and manufactured by the Aeromarine Plane and Motor Co.
Development and design
The PG-1 was intended to fulfill both ground strafing and aerial defense roles, the contract for construction was won by Aeromarine in May 1921.[1]
Armed with a single 0.5 in (12.7 mm) machine gun as well as a 37 mm Baldwin cannon firing through the propeller hub; the cockpit had 1⁄4-inch (6.35 mm) armour. The wings were dissimilar, with a wide-chord upper wing with ailerons, and a closely spaced narrow-chord lower plane with dihedral that placed the tips close to the upper wing. The upper wing was mounted close to the top of the fuselage with a cut-away forward section to accommodate the cockpit, and attached to the lower plane via V-type struts.[1]
Power was to have been provided by the eight-cylinder, water-cooled 330 hp (250 kW) Wright K-2 engine but the first two prototypes were fitted with 346 hp (258 kW) Packard 1A-1116 units due to delays in clearing the K-2 for flight testing.[1] A third prototype was also built and testing was eventually carried out using both the K-2 and Packard 1A-1237 at McCook Field.[1] Prototype aircraft suffered disappointing performance, high levels of vibration and poor visibility. The aircraft had a tendency to spin when stalled.[2] Development was abandoned in 1922.[1]
Specifications
Data from Angelucci, 1987. pp. 35-36.[1]
General characteristics
- Crew: 1
- Length: 24 ft 6 in (7.47 m)
- Wingspan: 40 ft 0 in (12.19 m)
- Height: 8 ft 0 in (2.44 m)
- Wing area: 389 sq ft (36.1 m2)
- Empty weight: 3,030 lb (1,374 kg)
- Gross weight: 3,918 lb (1,777 kg)
- Powerplant: 1 × Packard 1A-1116 , 346 hp (258 kW)
Performance
- Maximum speed: 130 mph (210 km/h, 110 kn)
- Range: 195 mi (314 km, 169 nmi)
- Service ceiling: 19,000 ft (5,800 m)
- Rate of climb: 684 ft/min (3.47 m/s)
Armament
- Guns: 1x 37 mm (1.457 in) Baldwin cannon + 1x 0.50 in (12.7 mm) machine gun
References
Notes
Bibliography
- Angelucci, Enzo (1987). The American Fighter from 1917 to the present. New York: Orion Books. p. 36.
- Green, W. & Swanborough, G. (1994). The Complete Book of Fighters. London: Salamander Books. ISBN 1-85833-777-1
This page was last edited on 1 August 2022, at 01:56