User:TheLongTone/Blériot-SPAD S.45

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[3]


S.45
Role Passenger aircraft
National origin France
Manufacturer Blériot Aéronautique
Designer Andre Herbemont

The Blériot-SPAD S.45 was a passenger aircraft built by () in 1921.

circular section monocoque fuselage constructed of three layers of plywood.

It was powered by four 220 kW (300 hp) Hispano-Suiza engines. These were mounted in a pair of laminated wood nacelles mounted on the lower wing, each containing two engines mounted in tandem, one driving a tractor propeller and the other a pusher propeller

Pilot and flight engineer sat side-by-side in an open cockpit immediatly in front of the passenger compartment, with the navigator#wireless operator occupying a compartment in the extreme nose of the aircraft.[1]

Exhibited in an unfinished condition at the 1921 Paris Aero Salon

Difficulty in carrying out static load testing on the monocoque fuselage delayed the granting of a certificate of airworthiness[2]

Specifications[edit]

Data from [3]

General characteristics

  • Crew: 3
  • Capacity: 17
  • Length: 5.79 m (51 ft 10 in)
  • Upper wingspan: 21.46 m (70 ft 5 in)
  • Lower wingspan: 19.69 m (64 ft 7 in)
  • Height: 5.74 m (18 ft 10 in)
  • Powerplant: 4 × Hispano-Suiza piston engine, 220 kW (300 hp) each

Performance

  • Maximum speed: 200 km/h (124 mph, 108 kn) (estimated)

References[edit]

  1. ^ [1] Flight 24 Nov 1921
  2. ^ "Que Sont Devenus les Appareils du Dernier Salon?". 1 December1922: 272. {{cite journal}}: Check date values in: |date= (help); Cite journal requires |journal= (help)
  3. ^ [2] Flight 24 Nov 1921