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The fuel tanks were moved to the outer wings, fuel lines for a 330 L (87 US gal) drop tank were installed under each wing and the internal fuel capacity was increased to 570 L (150 US gal). More importantly, it regained its capabilities for long operating ranges, similar to the previous A6M2 Model 21, which was vastly shortened by the Model 32.
The Type 10 started as the TK-X (MBT-X) project, intended to complement and eventually replace the Type 74 and Type 90 tanks in service with the JGSDF. [5] Development began in the 1990s, and production started in 2010–2011.
A self-sealing fuel tank (SSFT) is a type of fuel tank, typically used in aircraft fuel tanks or fuel bladders, that prevents them from leaking fuel and igniting after being damaged. Typical self-sealing tanks have layers of rubber and reinforcing fabric, one of vulcanized rubber and one of untreated natural rubber, which can absorb fuel when ...
Further fuel tanks were situated in the thin wings both inboard and outboard of the engines, giving a total fuel capacity of 1,490 L (328 imperial gallons). The engines, two Mitsubishi Ha-26s, were housed in close fitting cowlings developed by the Aeronautical Research Institute of the Tokyo Imperial University to reduce drag and improve pilot ...
The Mitsubishi team continued to improve the A5M, working through versions until the final A5M4, which carried an external underside drop tank to provide fuel for extended range. The A5M's most competitive adversary in the air was the Polikarpov I-16 , a fast and heavily armed fighter flown by both Chinese Air Force regulars and Soviet volunteers.
The JH4 was an F-head engine based on the Willys Hurricane engine and its predecessor Willys Go-Devil sidevalve four, and was used to power early Mitsubishi Jeeps as well as Mitsubishi Fuso trucks and buses. It was of 2.2 L (2,199 cc), had 69 HP and formed the basis for the KE31, a diesel engine of the same dimensions.