Blériot-SPAD S.51
| S.51 | |
|---|---|
| Role | Fighter |
| Manufacturer | Blériot |
| Designer | André Herbémont |
| First flight | 16 June 1924 |
| Primary users | Polish Air Force Turkish Air Force Soviet Air Force |
| Number built | ca. 60 |
The Bleriot-SPAD S.51 was a French fighter aircraft developed in 1924 in response to a French Air Force requirement for an aircraft to replace their obsolete Nieuport-Delage NiD.29s.
Design and development
Designed by André Herbémont, the S.51 shared its basic configuration with his other aircraft of the period, being a biplane with a swept upper wing and unswept lower wing, joined by I-shaped interplane struts. The S.51, however, marked Herbémont's transition from a covered framework fuselage design to a monocoque fuselage.
The prototype S.51 was rejected by the French authorities, but revised versions found export customers in the Polish Air Force, which bought 50 of them, and the Turkish and Soviet air forces which each bought a single example. Another development, the S.51/3 was experimentally fitted with the first controllable pitch propeller developed in France, also designed by Herbémont.
Variants
- S.51/1
- Prototype for French evaluation.
- S.51/2
- Refined version exported to Poland.
- S.51/3
- Prototype with variable-pitch propeller.
- S.51/4
- Export version for Turkey and the USSR with two extra machine guns in the wings.
Operators
- Polish Air Force
- 11th (Kosciusko) Squadron
Specifications (S.51/2)
General characteristics
- Crew: one pilot
Performance
References
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 164.
- World Aircraft Information Files. London: Bright Star Publishing. pp. File 890 Sheet 42.
- aviafrance.com
See also