Besson MB.26
The Beeson MB.26 was a French sesquiplane floatplane designed by Marcel Besson as a shipborne two-seat reconnaissance aircraft for the French Navy, but it was not ordered into production.[1]
MB.26 | |
---|---|
![]() | |
Role | Reconnaissance or fighter floatplane |
National origin | France |
Manufacturer | Besson |
Designer | Marcel Besson |
First flight | 1925 |
Design and development
The MB.26 was a W-strut wing braced sesquiplane, the upper wing was attached at the top of the fuselage and the lower was below the fuselage.[1] It had one main float under the lower wing and two stabilizing floats on the wingtips.[1] This HB.2 variant was followed by a modified C.2 configuration to turn it into a two-seat fighter seaplane.[1] The C.2 had a new round-sided fuselage, the HB.2 had a slab-sided fuselage, and a new tailplane.[1] Neither variant was ordered or entered production.[1]
Variants
Specifications (HB.2)
Data from [1] The Illustrated Encyclopedia of Aircraft
General characteristics
- Crew: 2
- Length: 12.10 m (39 ft 8¼ in)
- Wingspan: 15.00 m (49 ft 2½ in)
- Height: 3.70 m (12 ft 1¼ in)
- Wing area: 52.00 m2 (559.74 ft2)
- Empty weight: 1665 kg (3671 lb)
- Gross weight: 2415 kg (5324 lb)
- Powerplant: 1 × Lorraine 12Db inline piston engine, 298 kW (400 hp)
Performance
- Maximum speed: 180 km/h (112 mph)
- Service ceiling: 5200 m (17060 ft)
Armament
- One fixed forward-firing 7.7mm (0.303in) machine-gun
- Twin 7.7mm (0.303in) machine-guns on ring-mount at observers cockpit
References
Notes
- Orbis 1985, p. 656
Bibliography
- The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.