Nakajima Ki-34
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| Ki-34 "Thora" | |
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Nakajima AT-2, civil version of the Ki-34 |
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| Type | Civil airliner/Light military transport |
| Manufacturer | Nakajima Aircraft Company |
| Maiden flight | 12 September 1936 |
| Introduced | 1937 |
| Primary users | IJA Air Force IJN Air Service Dai Nippon Koku KK Manchukuo National Airways |
| Number built | 351 |
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 of World War II assigned the type the code-name "Thora".
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[edit] Design and development
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 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 580 shp (430 kW) Nakajima Kotobuki 2-1 radial engines with fixed pitch wooden propellers, which were replaced in production models with Kotobuki-41 710 shp (530 kW) nine-cylinder radial engines, with variable pitch metal propellers.
[edit] Civil operational history (AT-2)
A total of thirty-two AT-2s were produced for Imperial Japanese Airways (Dai Nippon Koku KK) and Manchukuo National Airways,[1] 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.
[edit] Military operational history (Ki-34)
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. The designation was later changed to Ki-34. The initial 19 aircraft were produced by Nakajima Aircraft, and another 299 aircraft were subsequently produced by the Army-affiliated Tachikawa Aircraft Company Ltd. The final airframe was delivered in 1942.
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.
At a later date, some aircraft were transferred to the Imperial Japanese Navy, where they were known as the Navy Type AT-2 or Navy Type L1N1. Several were also transferred to the air force of the Japanese puppet state of Cochin China in 1942.
[edit] Operators
[edit] Military operators
[edit] Civil operators
- Imperial Japanese Airways (Dai Nippon Koku KK)
[edit] Specifications (Ki-34)
Data from Warbirds Resource Group[2]
General characteristics
- Crew: 2
- Capacity: 8 passengers
- Length: 15.30 m (59 ft 2.25 in)
- Wingspan: 19.81 m (65 ft 0 in)
- 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)
- Useful load: kg (kg)
- Max takeoff weight: 5,250 kg (lb)
- Powerplant: 2× Nakajima Kotobuki 9-cylinder, air-cooled radial, 529-kW (710-hp) each
Performance
- Never exceed speed: km/h (knots, mph)
- Maximum speed: 360 km/h (knots,)
- Cruise speed: 310 km/h (knots, mph)
- Stall speed: km/h (knots, mph)
- Range: 1,200 km (nm, 746 mi)
- Service ceiling 7,000 m (22,965 ft)
- Rate of climb: m/s (ft/min)
- Wing loading: kg/m² (lb/ft²)
- Power/mass: W/kg (hp/lb)
Armament none
[edit] References
- Wilson, Stuart (1999). Airliners of the World. Australian Aviation. ISBN: 1875671447.
[edit] External links
[edit] Notes
[edit] See also
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