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・ Tupolev ANT-37
・ Tupolev ANT-41
・ Tupolev ANT-7
・ Tupolev ANT-8
・ Tupolev ANT-9
・ Tupolev DB-1
・ Tupolev I-12
・ Tupolev I-14
・ Tupolev I-4
・ Tupolev I-8
・ Tupolev MTB-1
・ Tupolev MTB-2
・ Tupolev SB
・ Tupolev TB-1
・ Tupolev TB-3
Tupolev TB-6
・ Tupolev Tu-1
・ Tupolev Tu-102
・ Tupolev Tu-104
・ Tupolev Tu-107
・ Tupolev Tu-110
・ Tupolev Tu-114
・ Tupolev Tu-116
・ Tupolev Tu-12
・ Tupolev Tu-121
・ Tupolev Tu-123
・ Tupolev Tu-124
・ Tupolev Tu-125
・ Tupolev Tu-126
・ Tupolev Tu-134


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Tupolev TB-6 : ウィキペディア英語版
Tupolev TB-6

Tupolev TB-6 (internal designation ANT-26; (ロシア語:Туполев ТБ-6/АНТ-26)) was a proposal for a 1930s heavy bomber that did not advance beyond blueprints. Inspired by the success of ANT-20/PS-124, Tupolev in 1929 began work on an even larger aircraft powered by 12 engines and with a takeoff weight of . By the mid-1930s, the trend in military aviation shifted towards smaller and faster aircraft and the TB-6 was cancelled. ANT-28 was a proposed cargo version.
A 0.21:1 scale two-seat glider was built by AGOS (''() Aviatsii, Ghidroaviahtsii i Opytnovo Samolyotostroyeniya'' - (for ) aviation, hydro-aviation and experimental construction) and test-flown by B.N. Kudrin, to evaluate the aerodynamic soundness of the design before work was started on the first prototype.
==Specifications (TB-6 estimated)==


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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