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Ki-36
Tachikawa Ki-36 98chokkyo.jpg
Role Two-seat Army Co-operation Aircraft
Manufacturer Tachikawa Aircraft Company Ltd
First flight 20 April 1938
Primary users Imperial Japanese Army Air Force
Royal Thai Air Force
Produced 1938 - 1944
Number built 1,334
Variants Tachikawa Ki-55

The Tachikawa Ki-36 (named Ida in Allied reporting code) was a Japanese army cooperation aircraft of World War II. It was a two-seat, low-wing monoplane with a single piston-engine and a fixed, tailwheel-type undercarriage.

Design and developmentEdit

The prototype, fitted with a 450 hp (336 kW) Hitachi Army Type 98 Ha-13 engine, first flew on 20 April 1938. Having outperformed the Mitsubishi Ki-35 in comparative trials, the Ki-36 was designated the Army Type 98 Direct Co-operation Aircraft and ordered into production in November 1938. Production ended in January 1944 after a total of 1,334 had been built.

Operational historyEdit

The Ki-36 first saw action in China where it saw success. Later, in the Pacific, it proved excessively vulnerable to opposing fighters. It was thereafter redeployed to the safer theater of China. Towards the end of the war, the Ki-36 was employed as a kamikaze aircraft with a bomb of 500-kg (1,102-lb) fitted externally.[1]

VariantsEdit

  • Ki-55 : Trainer version.
  • Ki-72 : An evolved version with a 600-hp (447-kW) Hitachi Ha-38 engine and retractable undercarriage, not built.

OperatorsEdit

RTAF Tachikawa Ki-36

Tachikawa Ki-36 trainer at the Royal Thai Air Force Museum.

Flag of the People's Republic of China.svg People's Republic of China
Flag of Indonesia.svg Indonesia
Flag of Japan.svg Japan
Flag of Thailand.svg Thailand

Specifications (Ki-36)Edit

Data from Japanese Aircraft of the Pacific War;[1] The Concise Guide to Axis Aircraft of World War II[2]

General characteristics
  • Crew: 2
  • Length: 8.00m (25ft 3in)
  • Wingspan: 11.80m (38ft 8.5in)
  • Height: 3.64m (11ft 11.25in)
  • Wing area: 20m² (215.29ft²)
  • Empty weight: 1,247kg (2,749lb)
  • Loaded weight: 1,660kg (3,660lb)
  • Powerplant: 1 × Hitachi Army Type 98 Ha-13a nine cylinder air-cooled radial engine, 380kW (510hp)

Performance

  • Maximum speed: 348km/h (216mph)
  • Cruise speed: 235km/h (146mph)
  • Range: 1,235km (767mi)
  • Service ceiling: 8,150m (26,740ft)
  • Wing loading: 83kg/m² (17lb/ft²)
  • Power/mass: 0.23kW/kg (0.31hp/kg; 0.14hp/lb)
  • Time to 3000m (9,845ft): 6min 39sec</ul></ul>Armament
  • one fixed, forward-firing 7.7mm (0.303in) machine-gun , one flexible 7.7mm (0.303in) machine-gun in rear cockpit.
  • up to 150kg (331lb) external bombload.

See alsoEdit

ReferencesEdit

Notes
  1. 1.0 1.1 Francillon 1979, p. 253.
  2. Mondey 1996, p. 246.
Bibliography
  • Francillon, Ph.D., René J. Japanese Aircraft of the Pacific War. London: Putnam Aeronautical, 1987. ISBN 0-85177-801-1.
  • Mondey, David. The Concise guide to Axis Aircraft of World War II. London: Chancellor Press, 1996. ISBN 1-85152-966-7.
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External linksEdit

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