Download Heinkel He-162 by J. Richard Smith with William Conway PDF
By J. Richard Smith with William Conway
;Heinkel He-162 [Aircraft Profile 203] КНИГИ ;ВОЕННАЯ ИСТОРИЯ Название: Heinkel He-162 Автор: J. Richard Smith with William Conway Серия: plane Profile 203 Издательство: Profile guides Ltd Год издания: 1967 Страниц:12 Формат: PDF в rarЯзык: английский Размер: 10.82 Мб Для сайта: Мир книгВ конце Второй мировой Германия пыталась создать простой и дешевый истребитель, и им стал реактивный Heinkel He-162. Построенный в очень небольшом количестве, самолет не успел проявить себя в бояхifolder.ru.com zero
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Example text
43 G-2 G-2 tp G-4 tp G-5 K-1 G-6/U2 G-6 K-2 Ausgestellt am: Aussteller: Total 8 9 10 11 12 1 2 35 40 45 50 50 50 50 930 170 195 60 50 60 190 140 160 160 40 3 4 5 6 7 8 9 10 11 12 1 2 3 4 5 6 7 8 9 50 50 50 50 50 50 50 50 50 50 50 50 50 50 50 50 50 50 30 250 60 290 310 330 350 370 390 400 400 380 350 300 250 200 150 100 30 450 709! 430 7521 400 350 7921 8271 300 250 8571 882! 43 165 622 320 340 3851 4191 360 380 4551 4931 400 420 5331 5751 440 450 6191 6641 50 50 50 50 50 50 50 50 50 50 50 50 50 50 50 50 50 50 30 450 290 500 500 500 500 500 500 500 500 500 450 450 350 250 150 100 50 20 550 9281 550 9831 500 500 400 300 2(X) 150 UK) 50 10331 10831 11231 11531 11731 11881 11981 12031 200 210 240 250 1721 1931 2171 2421 260 270 2681 295!
The higher all-up weight meant that larger wheels were required. Lengthening of the ailerons and slats was also necessary. It was anticipated that extra fuel tanks would be installed in the second fuselage in place of the pilot seat. A new. rectangular horizontal tail likewise had to be produced. The rest would be taken from existing production. Armament for the destroyer role was to be five MK 108 canon or four MK 108s and one MK 103. The bomber version would carry a reduced armament of two MK 108s but would have increased fuel tankage of 1140 liters.
5 m/sec. 4 km. Range at that speed was 585 kilometers. Time to climb to 6 000 meters was 8 minutes. Maximum speed at emergency power was 580 kph at ground level and 710 kph at maximum boost altitude of 7 500 meters. Landing speed with a landing speed of 3 tons was 150 kph. The MW 50 system was also the subject of frequent discussion, for example, the question of dispensing with the overflow limiter in the MW 50 tank. On 26 June 1944 it was decided by C-E 2 III Bormann to proceed with the overflow limiter in the MW 50 tank in order to avoid further delays.