Samiksha Jaiswal (Editor)

Nakajima Ki 34

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Top speed
  
360 km/h

Length
  
15 m

Wingspan
  
20 m

Introduced
  
1937

Nakajima Ki-34 wwwaviastarorgpicturesjapannakajimaki34jpg

The Nakajima Ki-34 was a Japanese light transport of World War II. It was a twin-engine, low-wing monoplane; the undercarriage was of tailwheel type with retractable main units. During the Pacific War, the Allies assigned the type the reporting name Thora.

Contents

Nakajima Ki-34 Japan39s Nakajima Ki34 transport

Design and development

Nakajima Ki-34 TheBlueprintscom Blueprints gt WW2 Airplanes gt Nakajima

The Ki-34 was originally designed as a civil transport. Nakajima Aircraft Company, which had the license-production rights to the Douglas DC-2, began design work in 1935 on a smaller twin engine airliner for routes which did not have the capacity to justify use of the larger DC-2. The initial design was designated AT-1, and after numerous design iterations, flew as a prototype designated AT-2 on 12 September 1936. The design was all metal, except for the flight control surfaces, which were plywood. The wings used a multi-cell cantilever design. The prototype was fitted with 432 kW (580 hp) Nakajima Kotobuki 2-1 radial engines with fixed pitch wooden propellers, which were replaced in production models with Kotobuki-41 529 kW (710 hp) nine-cylinder radial engines, with variable pitch metal propellers.

Civil use (AT-2)

Nakajima Ki-34 Nakajima Ki34 L1N1 THORA passenger transport

A total of 32 AT-2s were produced for Imperial Japanese Airways (Dai Nippon Koku KK) and Manchukuo National Airways, operating on scheduled routes between Tokyo and Hsinking, Tokyo and Tianjin, and within Manchukuo. These aircraft remained in operational service until the surrender of Japan in August 1945.

Military history (Ki-34 and L1N1)

Nakajima Ki-34 Nakajima Ki34 Wikipedia

With a high demand for increased military transport capability after the start of the Second Sino-Japanese War in 1937, the Imperial Japanese Army adapted the AT-2 design for military use by fitting with more powerful Nakajima Ha-1b radial engines and re-designating the aircraft as the Army Type 97 Transport and Ki-34. The initial 19 aircraft were produced by Nakajima Aircraft, and another 299 aircraft were subsequently produced by the Army-affiliated Tachikawa Hikoki K.K.. The final airframe was delivered in 1942.

Nakajima Ki-34 Nakajima Ki34 Type 97 Thora Info

In operational service, the Ki-34 was used as a utility aircraft for liaison and communications duties, and for paratrooper training and Special Forces operations.

Nakajima Ki-34 Nakajima Ki34 Type 97 Thora Info

At a later date, some aircraft were transferred to the Imperial Japanese Navy, where they were known as the Navy Type AT-2 Transport or Nakajima L1N1. Several were also transferred to the air force of the Japanese puppet state of Cochinchina in 1942.

Military operators

China-Nanjing
  • Nanjing air force
  •  Japan
  • Imperial Japanese Army Air Force
  • Imperial Japanese Navy Air Service
  • Civil operators

     Japan
  • Imperial Japanese Airways (Dai Nippon Koku KK)
  •  Manchukuo
  • Manchukuo National Airways
  •  Mongolia
  • Mongolian People's Army Aviation-Captured and operated more than 12 aircraft since in late September 1945
  • Specifications (Ki-34)

    Data from Japanese Aircraft of the Pacific War; Warbirds Resource Group

    General characteristics

  • Crew: 3
  • Capacity: 8 passengers
  • Length: 15.30 m (59 ft 2.25 in)
  • Wingspan: 19.81 m (65 ft)
  • Height: 4.15 m (13 ft 7.5 in)
  • Wing area: 49.2 m² (529.6 ft²)
  • Empty weight: 3,500 kg (7,716 lb)
  • Loaded weight: 5,250 kg (11,574 lb)
  • Powerplant: 2 × Nakajima Kotobuki 2-1 nine cylinder, air-cooled radial engine, 529 kW (710 hp) each
  • Performance

  • Maximum speed: 360 km/h (194 kn, 224 mph)
  • Cruise speed: 310 km/h (167 kn, 193 mph)
  • Range: 1,200 km (648 nmi, 746 mi)
  • Service ceiling: 7,000 m (22,965 ft)
  • Wing loading: 106.7 kg/m² (21.9 lb/ft²)
  • Armament

    none

    References

    Nakajima Ki-34 Wikipedia