type of aircraft
Savoia-Marchetti SM.91
The Savoia-Marchetti SM.91 was a two-seat, twin-engined, Italian heavy fighter prototype, designed to compete in a 1942 revision to a long-range fighter-bomber contract offered by the Regia Aeronautica to Italian aircraft companies in 1938. The original 1938 specification yielded the Savoia-Marchetti SM.88, which the SM.91 was largely based on.
Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.
- Manufacturer
- SIAI-Marchetti
- First flight
- 1943-03-11
Specifications
- Cruise speed
- 278 kt
- Max speed
- 315 kt
- Range
- 860 nm
- Service ceiling
- 36,000 ft
- Max takeoff weight
- 19,600 lb
- Empty weight
- 14,110 lb
- Fuel capacity
- 420 US gal
- Powerplant
- 2 × Daimler-Benz DB 605A-1
- Engines
- 2
- Seats
- 2
- Length
- 43.5 ft
- Wingspan
- 64.7 ft
- Height
- 12.7 ft
- Number built
- 2
Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).
Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.