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・ Junkers Ju 187
・ Junkers Ju 188
・ Junkers Ju 252
・ Junkers Ju 268
・ Junkers Ju 287
・ Junkers Ju 288
・ Junkers Ju 290
・ Junkers Ju 322
・ Junkers Ju 352
・ Junkers Ju 388
・ Junkers Ju 390
・ Junkers Ju 46
・ Junkers Ju 488
・ Junkers Ju 49
・ Junkers Ju 52
Junkers Ju 60
・ Junkers Ju 86
・ Junkers Ju 87
・ Junkers Ju 88
・ Junkers Ju 89
・ Junkers Ju 90
・ Junkers Jumo 004
・ Junkers Jumo 204
・ Junkers Jumo 205
・ Junkers Jumo 210
・ Junkers Jumo 211
・ Junkers Jumo 213
・ Junkers Jumo 222
・ Junkers Jumo 223
・ Junkers K 16


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Junkers Ju 60 : ウィキペディア英語版
Junkers Ju 60
__NOTOC__

The Junkers Ju 60 was a single engine airliner built in prototype form in Germany in the early 1930s. It was designed to meet a requirement issued by the ''Reichsverkehrministerium'' (Reich Transport Ministry) for a German-built equivalent to the Lockheed Vega with which to equip Deutsche Luft Hansa. The result was a sleek, cantilever monoplane of conventional configuration, with wings skinned in the corrugated duralumin that had been a hallmark of Junkers designs up to this time, although this would be the last Junkers aircraft to have this feature. The main units of the tailwheel undercarriage were retractable.
The Ju 60 was evaluated by Deutsche Luft Hansa against the Heinkel He 70. With the latter able to demonstrate a top speed 75 km/h (47 mph) better than the Ju 60, development of the Junkers design was halted before the third prototype had been completed. The two examples that had already been constructed eventually saw service with the ''Luftwaffe'' as liaison aircraft until 1942. The work done on the design would later form the basis of the Ju 160.




==Specifications==


抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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