Manshū_Hayabusa

Manshū Hayabusa

Manshū Hayabusa

Japanese airliner


The Manshū MT-1 Hayabusa (Japanese: 隼, "Peregrine Falcon") was an airliner produced by the Japanese Manchuria Airplane Manufacturing Company in Manchukuo in the late 1930s.[2][3] It was a conventional, low-wing cantilever monoplane with fixed tailwheel undercarriage. The flight deck was fully enclosed and separate from the passenger cabin, which could seat six people. The type equipped Manchukuo National Airways.

Quick Facts MT-1 Hayabusa, Role ...


Specifications (Production aircraft)

Data from Japanese Aircraft, 1910-1941[1]

General characteristics

  • Crew: 1 pilot
  • Capacity: 6 passengers
  • Length: 9.38 m (30 ft 9 in)
  • Wingspan: 13.60 m (44 ft 7 in)
  • Height: 3.60 m (11 ft 10 in)
  • Wing area: 27.3 m2 (294 sq ft)
  • Empty weight: 1,700 kg (3,748 lb)
  • Gross weight: 2,700 kg (5,952 lb)
  • Powerplant: 1 × Nakajima Kotobuki 2-kai-1 nine-cylinder air-cooled radial engine , 343 kW (460 hp)

Performance

  • Maximum speed: 240 km/h (150 mph, 130 kn)
  • Cruise speed: 200 km/h (120 mph, 110 kn)
  • Range: 902 km (560 mi, 487 nmi)
  • Service ceiling: 6,000 m (20,000 ft)

See also

Aircraft of comparable role, configuration, and era


References

Notes
Bibliography
  • The Illustrated Encyclopedia of Aircraft. London: Aerospace Publishing.
  • Mikesh, Robert C.; Abe, Shorzoe (1990). Japanese Aircraft 1910-1941. London: Putnam Aeronautical Books. ISBN 0-85177-840-2.
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.
  • Bueschel, Richard (May 1961). "The Mansyu Hayabusa". Air Pictorial.

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