Pilatus P-1
From Wikipedia, the free encyclopedia
The Pilatus P-1 was a single-engined, single-seat training aircraft project from Pilatus Aircraft in Switzerland ca.1941.[1]
Design and development
The P-1 project began around the end of October 1940 as the first project of Pilatus, influenced by engineer Henri Fiert. The layout and design principles were carried through to the Pilatus P-2, which achieved success as a trainer with the Swiss Air Force. The fuselage structure of the P-1 would have consisted of welded steel tube, with removable front Aluminium alloy panels and fabric covering aft of the cockpit. The wings would have been of wood built up around a one-piece wooden spar with plywood skinning.[2]
Specifications (P-1 estimated)
Data from Pilatus Flugzeuge: 1939–1989[2]
General characteristics
- Crew: 1
- Length: 6.9 m (22 ft 8 in)
- Wingspan: 9.2 m (30 ft 2 in)
- Height: 2.1 m (6 ft 11 in)
- Wing area: 12.7 m2 (137 sq ft)
- Empty weight: 850 kg (1,874 lb)
- Gross weight: 1,150 kg (2,535 lb)
- Powerplant: 1 × Argus As 10E2 V-8 inverted air-cooled piston engine, 180 kW (240 hp)
Performance
- Maximum speed: 325 km/h (202 mph; 175 kn)
- Service ceiling: 6,000 m (19,685 ft)
- Rate of climb: 6.5 m/s (1,280 ft/min)
See also
- Related development
- Aircraft of comparable role, configuration and era
Notes
- ↑ Pilatus Chronik (in German). Stans: Pilatus. 2011. p. 1.
- ↑ 2.0 2.1 Eichenberger, Roland (1989). Pilatus Flugzeuge: 1939–1989 (in German). Stans: Pilatus Flugzeugwerk.
References
 |
Wikimedia Commons has media related to Pilatus Aircraft. |
- Eichenberger, Roland (1989). Pilatus Flugzeuge: 1939–1989 (in German). Stans: Pilatus Flugzeugwerk.
- Pilatus Chronik (in German). Stans: Pilatus. 2011. p. 1.
| ||||||||||||||
This article is issued from Wikipedia. The text is available under the Creative Commons Attribution/Share Alike; additional terms may apply for the media files.