By FRANCIS GALLEMI

Книга Warbird Profile No.1: A-26 B/C Invader Warbird Profile No.1: A-26 B/C Invader Книги Вооружение Автор: Francis Gallemi Год издания: 1994 Формат: pdf Издат.:Aries guides Страниц: forty four Размер: 16.65 ISBN: 0969857802 Язык: Английский0 (голосов: zero) Оценка:The unique USAAF requisites known as for a multi objective assault plane that may be swifter than the B-26 Marauder, could hold a better bomb potential than the B-25 Mitchell and be extra manoeuvrable than the A-20 Havoc. the outcome was once the A-26 Invader, a extra powerfull, speedier and extra devastating warmachine than it really is predecessors it was once destined to interchange.

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67 kts) lAS; the flights took place on 7th October, 26th October and 13th November respectively. The aircraft was flown by test pilot Maj. V. G. Ivanov. On the whole the ejection system and the ejection seat received a positive assessment from the military who recommended them for use on production aircraft. Besides the ejection seat, wing-mounted airbrakes and auxiliary fuel tanks underwent State acceptance trials at GK Nil WS on the UTI MiG-9. Nevertheless, the sparka itself was not put into production.

The single-engined derivative of the MiG-9 was never flown. 38 Above: Close-up of the 1-305's weapons arrangement with all three cannons located in the horizontal plane. This MiG-9 had a centre cannon fitted with a lengthened barrel in yet another attempt to cure the engines' tendency to flame out when the cannons were fired. a. a. a. a. a. a. a. a. a. a. a. a. a. a. a. a. a. a. a. a. 0 and fitted with a standard armament fit were series-produced for some time. The table on this page illustrates the dimensions and performance of MiG-9 fighters with afterburning engines as recorded during manufacturer's flight tests.

A. a. a. 1,300 (2,866) n,a. a. 0) n,a. a. 3) n,a. n,a. a. a. a. a. 35 18,5 (3,640,8) 1,700 (? a. 4) 14,000 (45,931) 830 (515) 640 (2,099) 920 (3,018) 1x37 2 x23 Length (without armament) Height on ground Wing span Wing area, m' (sq It) All-up weight, kg (Ib): normal maximum Fuel load, kg (Ib) Top speed, km/h (kts): at sea level at 3,000 m(9,842 It) at 5,000 m(16,404 It) Landing speed, km/h (kts) Climb time to 5,000 m (16,404 It), minutes Rate of climb at S/L, m/sec (It/min) Service ceiling, m(It) Maximum range, km (miles) Take-off run, m(It) Landing run, m(It) Armament (calibre, mm) Notes: 1.

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