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・ Grigoriy Krivosheyev
・ Grigoriy Lvovitch Bondarevsky
・ Grigoriy Matuzkov
・ Grigoriy Mihaylovich Naginskiy
・ Grigoriy Myasoyedov
・ Grigoriy Oparin
・ Grigoriy Oster
・ Grigoriy Rechkalov
・ Grigoriy Suk
・ Grigoriy Yablonsky
・ Grigoriy Yegorov
・ Grigoropolisskaya
・ Grigorov Glacier
・ Grigorovich
・ Grigorovich (design bureau)
Grigorovich DI-3
・ Grigorovich I-1
・ Grigorovich I-2
・ Grigorovich I-Z
・ Grigorovich IP-1
・ Grigorovich M-1
・ Grigorovich M-11
・ Grigorovich M-15
・ Grigorovich M-16
・ Grigorovich M-24
・ Grigorovich M-5
・ Grigorovich M-9
・ Grigorovich SUVP
・ Grigorovich TB-5
・ Grigory


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Grigorovich DI-3 : ウィキペディア英語版
Grigorovich DI-3


Grigorovich DI-3 ((ロシア語:Григорович ДИ-3)), (''Dvukhmyestnyi Istrebitel'' - two-seat fighter), was a prototype two-seat fighter developed in the Soviet Union in the 1930s. It was intended to be a long-range escort fighter developed from the DI-2 with improved range and performance comparable to single-seat fighter aircraft of the time. DI-3 was a single-bay biplane of mixed construction with a twin-rudder tailplane of variable incidence. Although initial tests demonstrated flight characteristics comparable to Polikarpov I-5, the addition of armament and operational equipment caused significant degradation in performance and DI-3 did not enter mass production. The prototype was subsequently fitted with an enclosed cockpit and used as a VIP transport.
==Specifications (DI-3)==


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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