Dewoitine D.7
| D.7 | |
|---|---|
| |
| Role | ultralight sport plane |
| Manufacturer | Dewoitine |
| Designer | Emile Dewoitine |
| First flight | c.1924 |
| Number built | ~5-10 |
The Dewoitine D.7 was a French sport plane built in the mid 1920s.
Development
[edit]The D.7 was a conventionally laid-out monoplane, with a thick cantilever shoulder wing. Its single seat, open cockpit, provided with a small windscreen, was over the wing. It had conventional, fixed, tailskid landing gear.
The D.7 could be powered by any small engine; the Salmson AD.3 radial engine, the Clerget 2K flat twin, Vaslin flat-four or Vaslin water-cooled six cylinder inline engines were fitted.
Operators
[edit]
- One aircraft was sold to the Japanese Army.
Specifications (AD.3 engine)
[edit]General characteristics
- Crew: 1
- Length: 5.60 m (18 ft 4.5 in)
- Wingspan: 12.60 m (41 ft 4 in)
- Wing area: 15.00 m2 (161.46 sq ft)
- Gross weight: 250 kg (551 lb)
- Powerplant: 1 × Salmson 3Ad three-cylinder radial engine , 9.0 kW (12 hp)
Performance
- Maximum speed: 90 km/h (56 mph, 49 kn)
- Endurance: 5 hours
- Service ceiling: 3,000 m (9,840 ft)
References
[edit]
Wikimedia Commons has media related to Dewoitine D.7.
- Donald, David, ed. (1997). The Encyclopedia of World Aircraft. Prospero Books. p. 333. ISBN 1-85605-375-X.
{{cite encyclopedia}}: Missing or empty|title=(help) - Aviafrance website/Dewoitine
 | This article on an aircraft of the 1920s is a stub. You can help Wikipedia by expanding it. |