Ki-56 Thalia
Transport Aircraft
Kawasaki
In the 30s, the United States was the undisputed leader in the commercial aircraft industry, creating a series of Douglas DC-2 and DC-3 passenger aircraft and transport aircraft and the Lockheed Electra high-speed aircraft. In early 1939, by order of the army, the Tachikawa company entered into a licensing agreement with Lockheed for the production of American aircraft in Japan. The model "Super Electra" L14-WG3B was used as a sample.
"Type Lo" Thelma. In 1940, the aircraft was adopted by the Japanese army under the designation "Type Lo Transport aircraft" *. Structurally, the aircraft was a twin-engine monoplane of an all-metal structure with retractable landing gear.
The Japanese car turned out to be identical to the American one, while the Japanese 14-cylinder radial engines Mitsubishi Ha-26-I, 10 hp, were installed on it. from. exceeding the power of the American Wright GR-1820-G3B, but in comparison with the American ones with more weight.
Since January 1941, the production of an early version of the "Type Lo" at Kawasaki was phased out after the release of 55 copies and the plant completely switched to production of the Ki-56. Production of "Type Lo" at Tachikawa continued until 1942 and ended with the release of only 45 copies, ie. a total of 100 Type Lo aircraft were produced.
Ki-56 Thalia. The production of the aircraft was additionally launched at the Kawasaki company. Takeo Doi took over the improvement of the aircraft on Kawasaki. The weight of the wing structure was reduced, the Fowler flaps were redesigned. The length of the fuselage was increased by 1.5 m with an increase in capacity to 16 passengers or 14 soldiers or 10 paratroopers. A large cargo hatch with a door was installed on the left side, a cargo winch was placed in the cabin, the aircraft could carry up to 2,400 kg of cargo. The power plant became more powerful and consisted of two Nakajima Na-25 engines of 990 hp each. Two prototypes were ready by the fall of 1940, the aircraft was designated Ki-56.
Production of the Ki-56 at Kawasaki continued until the summer of 1943. A total of 121 Ki-56s were produced, including two prototypes.
* Note admin. - under the abbreviation "Lo" was designated the firm Lockheed, which is the copyright holder for the design of the Japanese aircraft.
Kawasaki |
Тип "Ро" |
Ki-56 |
Crew |
3 |
3-4 |
Dimensions |
Wing span, m |
19.96 |
Wing area, m² |
51.19 |
51.20 |
Length, m |
13.51 |
14.90 |
Height, m |
3.48 |
3.60 |
Powerplant |
2×PE |
Na-26-I |
Na-25 |
power, hp |
2×850 |
2×990 |
Weights and loads, kg |
Empty weight |
4870 |
4672 |
Loaded weight |
7900 |
8030 |
Performance |
Maximum speed at altitude, km/h |
418 |
398 |
Cruising speed, km/h |
360 |
367 |
Rate of climb, m/min |
|
237 |
Service ceiling, m |
7500 |
Service range, km |
3400 |
3300 |
Payload, passengers |
10-12 |
14 |
|