Blériot-SPAD S.70
| S.70 | |
|---|---|
| Role | Fighter |
| Manufacturer | Blériot |
| Designer | André Herbemont |
| First flight | 20 April 1927 |
| Primary user | Aéronautique Militaire |
| Number built | 1 |
The Blériot-SPAD S.70 was a French fighter aircraft developed in the late 1920s.
Design and development[edit]
The S.70 was the second prototype of the S.60, being a two-seat biplane fighter of all-wood construction with a canvas coating and a monocoque fuselage.
Specifications[edit]
Data from [1]
General characteristics
- Crew: 1
- Length: 7.5 m (24 ft 7 in)
- Wingspan: 11.3 m (37 ft 1 in)
- Wing area: 36.6 m2 (394 sq ft)
- Empty weight: 1,331 kg (2,934 lb)
- Gross weight: 1,893 kg (4,173 lb)
- Powerplant: 1 × Lorraine 12Ed 'Courlis' W-12 water-cooled piston engine, 340 kW (450 hp)
- Propellers: 2-bladed fixed-pitch propeller
Performance
- Maximum speed: 210 km/h (130 mph, 110 kn)
See also[edit]
Related development
References[edit]
- ^ "SPAD S-70 - avion de chasse - Un siècle d'aviation française". Aviafrance.com. Retrieved 2019-02-03.