Standard E-1
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E-1 | |
---|---|
Type | Military trainer |
National origin | United States of America |
Manufacturer | Standard Aircraft Corporation |
Maiden flight | 1917 |
Primary user | United States Army Air Service |
Number built | 168 |
The Standard E-1 was an early American Army fighter aircraft, tested in 1917.
Built by the Standard Aircraft Corporation, the E-1 was an open-cockpit single-place tractor biplane, powered by an 80 hp (60 kW) Le Rhône or 100 hp (75 kW) Gnome or rotary engine. It proved unsuitable as a fighter, but about one hundred were bought as an advanced trainer; about half were completed as M-Defenses, being fitted as gunnery trainers. After World War One, three were modified as RPVs.
[edit] Specifications
General characteristics
- Crew: One pilot
- Length: 18 ft 5 in (5.61 m)
- Wingspan: 24 ft 0 in (7.31 m)
- Empty weight: 368 lb (811 kg)
- Gross weight: 1,140 lb (520 kg)
- Powerplant: 1 × Le Rhône rotary, 80 hp (60 kW)
Performance
- Maximum speed: 100 mph (160 km/h)
- Range: 180 miles (290 km)
- Service ceiling: 14,500 ft (4,420 m)
[edit] See also
Related lists
[edit] References
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions, 839.
- Donald, David, ed. Encyclopedia of World Aircraft, p.854, "Standard aircraft". Etobicoke, Ontario: Prospero Books, 1997.
- aerofiles.com
[edit] External links
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- This page contains material originally created for Standard E-1