MOMENTAN AUSVERKAUFT
Über dieses Produkt
Product Identifiers
PublisherKangero, Oficyna Wydawnicza
ISBN-10836667391X
ISBN-139788366673915
eBay Product ID (ePID)5057272873
Product Key Features
Book TitleMikoyan-Gurevich Mig-3 : Volume II
Number of Pages72 Pages
LanguageEnglish
Publication Year2022
TopicMilitary Science, Military / World War II, Models, Military / Aviation
IllustratorYes
GenreTechnology & Engineering, Crafts & Hobbies, History
AuthorDariusz Paduch
Book SeriesMonographs
FormatTrade Paperback
Dimensions
Item Length11.7 in
Item Width8.3 in
Additional Product Features
Intended AudienceTrade
Dewey Edition23
ReviewsThis book, coupled with the first volume, provides a very thorough picture of the MiG-3's development and production., There are some very good archive photos showing great detail on the type, accompanied with some drawings of detail elements which came from original manuals.
TitleLeadingThe
Series Volume Number3083
Dewey Decimal623.7464
SynopsisThe I-200 fighter project was a compromise between design office's capabilities, realities of the Soviet aviation industry, with its available technologies, and military requirements. According to the brief description of the MiG-3 from 1941, it was, in terms of its purpose, an interceptor, but, interestingly, it could also be used as... an attack aircraft, or a light, fast dive bomber. Both the I-200 prototypes and the later MiG-1 and MiG-3 were single-seat, single-engine, mixed-design low-wing aircraft. Front part of the fuselage, together with the center wing, up to the rear wall of the pilot's cockpit, was made of metal. Only the tail part of the fuselage and wing consoles were wooden. Vertical stabilizer, which was an integral part of the fuselage, was made of wood, too, but horizontal stabilizer was all-metal. Rudders and ailerons had a metal construction and canvas cover. Undercarriage was made of chromansil steel. In front part of the fuselage there was a pilot's cabin with a seat, instrument panel and controls, front fuel tank, main offensive armament, water cooler and other components. Center wing was attached to the front part of the fuselage at seven points, the rear part at four points, while the engine mount was supported by two., The I-200 fighter project was a compromise between design office's capabilities, realities of the Soviet aviation industry, with its available technologies, and military requirements.
LC Classification NumberUG1242.F5
