翻訳と辞書
Words near each other
・ Mitsubishi Ichigokan Museum, Tokyo
・ Mitsubishi J2M
・ Mitsubishi J4M
・ Mitsubishi J8M
・ Mitsubishi K3M
・ Mitsubishi K7M
・ Mitsubishi Ka-8
・ Mitsubishi Kasei
・ Mitsubishi KE engine
・ Mitsubishi Ki-1
・ Mitsubishi Ki-15
・ Mitsubishi Ki-18
・ Mitsubishi Ki-2
・ Mitsubishi Ki-20
・ Mitsubishi Ki-21
Mitsubishi Ki-30
・ Mitsubishi Ki-33
・ Mitsubishi Ki-46
・ Mitsubishi Ki-51
・ Mitsubishi Ki-57
・ Mitsubishi Ki-67
・ Mitsubishi Ki-83
・ Mitsubishi Kinsei
・ Mitsubishi Lancer
・ Mitsubishi Lancer (A70)
・ Mitsubishi Lancer Evolution
・ Mitsubishi Lancer Evolution X
・ Mitsubishi Lancer WRC
・ Mitsubishi Logistics
・ Mitsubishi Magna


Dictionary Lists
翻訳と辞書 辞書検索 [ 開発暫定版 ]
スポンサード リンク

Mitsubishi Ki-30 : ウィキペディア英語版
Mitsubishi Ki-30

The was a Japanese light bomber of World War II. It was a single-engine, mid-wing, cantilever monoplane of stressed-skin construction with a fixed tailwheel undercarriage and a long transparent cockpit canopy. The type had significance in being the first Japanese aircraft to be powered by a modern two-row radial engine. During the war, it was known by the Allies by the name Ann.
==Design and development==
The Ki-30 was developed in response to a May 1936 Imperial Japanese Army specification to replace the Kawasaki Ki-3 light bomber with a completely indigenously designed and built aircraft. Mitsubishi and Kawasaki were requested to build two prototypes each by December 1936. The specification called for a top speed of at 3,000 m (9,840 ft); normal operating altitude from 2,000 m (6,560 ft) to 4,000 m (13,130 ft), the ability to climb to 3,000 m (9,840 ft) within eight minutes and an engine to be selected from the Mitsubishi Ha-6 radial, Nakajima Ha-5 radial, or Kawasaki Ha-9-IIb liquid-cooled inline engines, a normal bomb load of and a maximum of , one forward-firing machine gun and one flexible rearward-firing machine gun, the ability to perform 60° dives for dive bombing, and a loaded weight less than .
The first Mitsubishi prototype flew on 28 February 1937 powered by a Mitsubishi Ha-6 radial. Originally, designed with a retractable main landing gear, wind tunnel tests indicated that the gain in speed was minimal due to the landing gear's extra weight and complexity and a fixed arrangement with "spatted" main wheels was chosen instead. The wing was mounted at a point above the line of the aircraft's belly in order fully enclose the bomb bay within the fuselage. The pilot sat just above the leading edge of the wing, and the rear-gunner/radio-operator just behind the wing trailing edge, in a long "greenhouse" canopy which gave both crewmen excellent all-around vision. The Ha-6 engine drove a three-blade variable-pitch propeller.
A second prototype, fitted with the slightly more powerful Nakajima Ha-5 engine, was completed the same month. Although two months behind schedule and overweight, both prototypes met or exceeded every other requirement. The second prototype's top speed of at 4,000 m (13,130 ft) led the Imperial Japanese Army Air Force to place an order for 16 service trials machines. These were delivered in January 1938 and the result of the trials was that the Army ordered the Ki-30 into production in March under the designation Army Type 97 Light bomber.
Mitsubishi built 618 production machines through April 1940, and the 1st Army Air Arsenal (Tachikawa Dai-Ichi Rikugun Kokusho) built 68 more by the time production ceased in September 1941. Including prototypes, a total of 704 Ki-30s were built.

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
ウィキペディアで「Mitsubishi Ki-30」の詳細全文を読む



スポンサード リンク
翻訳と辞書 : 翻訳のためのインターネットリソース

Copyright(C) kotoba.ne.jp 1997-2016. All Rights Reserved.