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Tachikawa Ki 9

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Top speed
  
240 km/h

Length
  
7.9 m

First flight
  
January 7, 1935

Wingspan
  
10 m

Retired
  
1945

Tachikawa Ki-9 Tachikawa Ki9 SPRUCE trainer

Manufacturer
  
Tachikawa Aircraft Company

The Tachikawa Ki-9 (九五式一型練習機, Kyūgo-shiki ichigata renshuki) was an intermediate training aircraft of the Imperial Japanese Army Air Force built by Tachikawa Aircraft Company Ltd in the 1930s. It was known to the Allies under the nickname of "Spruce" during World War II.

Contents

Tachikawa Ki-9 WINGS PALETTE Tachikawa Ki9 Spruce Japan

Design and development

Tachikawa Ki-9 Japan39s Tachikawa Ki9 trainer quotSprucequot

The Ki-9 was a two-seat unequal wingspan biplane design. Tachikawa originally planned to use the same basic airframe for both basic training and intermediate training, differentiating the two models by the use of different engines. The prototype Ki-9 flew on 7 January 1935, powered by a 261 kW (350 hp) nine-cylinder Hitachi Ha-13a radial engine. The second prototype was identical, and the third prototype was powered by a 112 hp (80 kW) Nakajima NZ seven-cylinder radial engine. The third prototype exhibited stability problems due a center of gravity issue, and as a result the primary trainer model was abandoned and the Ki-9 was developed only for the intermediate trainer. Tachikawa subsequently developed the Ki-17 for the primary trainer role. The first production aircraft were delivered in 1935.

Operational history

Tachikawa Ki-9 FileTachikawa Ki9jpg Wikimedia Commons

The Ki-9 was introduced to service as the Army Type 95-1 Medium Grade Trainer Model A under the former aircraft naming nomenclature system. The first version had a complex split-axle landing gear with fairings over the top of the wheels. In 1939 this was modified and simplified, the fuselage slightly shortened and total weight reduced. The resulting Army Type 95-1 Model B or Ki-9-kai had improved maneuverability and flight characteristics. This version was quickly superseded by the Army Type 95-1 Model C, or Ki-9-otsu in full production.

Tachikawa Ki-9 httpsuploadwikimediaorgwikipediacommonsthu

Both versions were used widely for blind-flying training with a folding hood over the rear cockpit, and several were modified with a glazed canopy over the rear cockpit for use as a staff officer transport plane.

Tachikawa Ki-9 Tachikawa Ki9 Wikipedia

Some were pressed into service for use as Kamikaze aircraft in the closing days of the war, fitted with an oil drum filled with explosives or fuel in the rear cockpit.

Tachikawa Ki-9 Tachikawa Ki9 SPRUCE trainer

Production by Tachikawa totaled 2,395 aircraft, ending in 1942. At least another 220 Ki-9s were constructed by Tokyo Gasu Denki (also known as Gasuden) from 1943-1945.

The Ki-9 was also flown in wartime by Japanese satellite countries and postwar by the fledgling government of Indonesia, and captured units by the Republic of China.

Variants

  • Ki-9 (Army Type 95-1 Medium Grade Trainer Model A): Initial version two-seat intermediate trainer aircraft.
  • Ki-9-ko (Army Type 95-1 Medium Grade Trainer Model B): Improved version.
  • Ki-9-otsu (Army Type 95-1 Medium Grade Trainer Model C): Standard production version.
  • (World War II)

     Japan
  • Imperial Japanese Army Air Force
  • China-Nanjing
  • Reorganized Republic of China Air Force
  •  Manchukuo
  • Manchukuo Air Force
  •  Thailand
  • Royal Thai Air Force
  • (postwar)

     Indonesia
  • Indonesian Air Force
  •  Republic of China
  • Republic of China Air Force
  •  South Korea
  • Republic of Korea Air Force
  • Specifications (Ki-9 Model A)

    Data from Japanese Aircraft of the Pacific War

    General characteristics

  • Crew: two
  • Length: 7.9 m (25 ft 11 in)
  • Wingspan: 10.32 m (33 ft 10 in)
  • Height: 3.1 m (10 ft 2 in)
  • Wing area: 24.5 m² (264 ft²)
  • Empty weight: 1,120 kg (2,468 lb)
  • Max. takeoff weight: 1,580 kg (3,482 lb)
  • Powerplant: 1 × Hitachi Ha-13a radial engine, 261 kW (350 hp)
  • Performance

  • Maximum speed: 240 km/h (130 kn, 149 mph)
  • Cruise speed: 150 km/h (93 mph)
  • Service ceiling: 5,800 m (19,030 ft)
  • Wing loading: 58.2 kg/m² (11.9 lb/ft²)
  • Endurance: 3.5 hours
  • References

    Tachikawa Ki-9 Wikipedia