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Tachikawa Ki-55

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Article Genealogy
Parent: kamikaze Hop 4
Expansion Funnel Raw 34 → Dedup 17 → NER 4 → Enqueued 4
1. Extracted34
2. After dedup17 (None)
3. After NER4 (None)
Rejected: 13 (not NE: 13)
4. Enqueued4 (None)
Tachikawa Ki-55
NameTachikawa Ki-55
TypeAdvanced trainer
ManufacturerTachikawa Aircraft Company
DesignerRyokichi Endo
First flightSeptember 1939
Introduced1940
Retired1945
Primary userImperial Japanese Army Air Service
Number built1,389
Developed fromTachikawa Ki-36

Tachikawa Ki-55 was a single-engine, two-seat advanced trainer aircraft operated by the Imperial Japanese Army Air Service during the Second World War. Developed from the successful Tachikawa Ki-36 army cooperation aircraft, it was designed specifically for pilot instruction and was known to the Allies under the reporting name "Ida". The type was renowned for its docile handling characteristics and reliability, becoming a cornerstone of Japanese flight training throughout the conflict.

Development and design

The development of the Ki-55 was initiated by the Imperial Japanese Army Air Service to fulfill a requirement for a dedicated advanced trainer, leveraging the proven airframe of the Tachikawa Ki-36. Under the leadership of designer Ryokichi Endo at the Tachikawa Aircraft Company, the project focused on simplifying the Ki-36 for the training role. Key modifications included the removal of military equipment such as the bomb rack, reconnaissance camera, and the rear defensive machine gun, which reduced weight and complexity. The aircraft retained the all-metal construction and the reliable Hitachi Ha-13a radial engine, which produced 450 horsepower and drove a two-bladed propeller. The design emphasized stability and forgiving flight characteristics, essential for training novice pilots in techniques like landings, navigation, and formation flying before transitioning to frontline fighters like the Nakajima Ki-43.

Operational history

Entering service in 1940, the Ki-55 quickly became the standard advanced trainer for the Imperial Japanese Army Air Service, deployed at primary flight schools across the Japanese archipelago and in occupied territories such as Manchukuo and French Indochina. Throughout the Pacific War, it played a vital role in sustaining the flow of pilots to combat units, despite increasing Allied aerial supremacy and material shortages. While not designed for combat, some Ki-55s were occasionally pressed into light liaison or communications duties. In the final stages of the war, with Boeing B-29 Superfortress raids devastating Japanese industry and infrastructure, many trainers were destroyed on the ground. Surviving aircraft were scrapped following the surrender of Japan and the subsequent dissolution of the Imperial Japanese Army.

Variants

The Ki-55 production run was largely consistent, with only minor modifications throughout its manufacturing life. The sole designated variant was the Ki-55 KAI, which featured some aerodynamic refinements and equipment changes late in the war to simplify production. A proposed floatplane version, tentatively designated the Ki-72, was designed but never progressed beyond the project stage. The aircraft's direct predecessor, the Tachikawa Ki-36, remained in production as a separate type for army cooperation and light attack missions, seeing action in campaigns including the Second Sino-Japanese War and the Malayan campaign.

Operators

The primary and essentially sole operator of the Ki-55 was the Imperial Japanese Army Air Service. Following the war, a small number of captured aircraft were briefly evaluated by technical intelligence units of the United States Army Air Forces and the Royal Air Force. No Ki-55s were transferred to or used operationally by the air forces of any other nation, including Japan's Axis partners like Nazi Germany or the Kingdom of Italy.

Specifications (Ki-55)

* Crew: 2 (student and instructor) * Length: 8.00 m (26 ft 3 in) * Wingspan: 11.80 m (38 ft 9 in) * Height: 3.64 m (11 ft 11 in) * Wing area: 20.0 m² (215 sq ft) * Empty weight: 1,247 kg (2,749 lb) * Gross weight: 1,660 kg (3,660 lb) * Powerplant: 1 × Hitachi Ha-13a 9-cylinder air-cooled radial piston engine, 340 kW (450 hp) * Propellers: 2-bladed fixed-pitch propeller * Maximum speed: 348 km/h (216 mph, 188 kn) * Cruise speed: 235 km/h (146 mph, 127 kn) * Range: 1,060 km (660 mi, 570 nmi) * Service ceiling: 8,150 m (26,740 ft) * Rate of climb: 8.33 m/s (1,640 ft/min)

Category:Military trainer aircraft 1930–1939 Category:World War II Japanese trainer aircraft Category:Tachikawa aircraft Category:Single-engined tractor aircraft Category:Aircraft first flown in 1939