Tachikawa Ki-36
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Ki-36 | |
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Type | Two-seat Army Co-operation Aircraft |
Manufacturer | Tachikawa |
Maiden 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 (codenamed Ida in allied code) was a Japanese army-cooperation aircraft of the Second World War.
The Ki-36 was a two-seat, low-wing monoplane with a single piston-engine and a fixed, tailwheel-type undercarriage.
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[edit] Design and development
The prototype, fitted with a 450hp (336kW) Hitachi Ha13 engine, first flew on 20th 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.
[edit] Operational history
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 redeployed to the safer theatre of China.
Towards the end of the war, the Ki-36 was employed as a kamikaze with a bomb of 500-kg (1,102-lb) fitted internally.
[edit] Variants
- Ki-55
- Trainer version.
- Ki-72
- An evolved version with a 600-hp (447-kW) Hitachi Ha-38 engine and retractable undercarriage, not built.
[edit] Operators
- Chinese Communist Air Force operated 2 captured aircraft postwar as trainers until their retirement in early 1950s.
- Indonesian People's Security Force
[edit] Specifications (Ki-36)
Data from The Concise Guide to Axis Aircraft of World War II [1]
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: kg (lb)
- Useful load: kg (kg)
- Max takeoff weight: 1,660kg (3,660lb)
- Powerplant: 1× Hitachi Ha-13a 9-cylinder radial 2, 380kW (510hp)
Performance
- Never exceed speed: km/h (knots, mph)
- Maximum speed: 348km/h (knots, 216mph)
- Cruise speed: 235km/h (knots, 146mph)
- Stall speed: km/h (knots, mph)
- Range: 1,235km (nm, 767mi)
- Service ceiling 8,150m (26,740ft)
- Rate of climb: m/s (ft/min)
- Wing loading: kg/m² (lb/ft²)
- Power/mass: W/kg (hp/lb)
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.
[edit] References
[edit] Notes
- ^ Mondey 1996, p.246.
[edit] Bibliography
- Francillon, 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, 1996. ISBN 1 85152 966 7.
[edit] See also
Related development Tachikawa Ki-55
Related lists
[edit] External links
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