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hardy
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tarasv
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21.05.2008 22:20:27
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Рубрики
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WWII;
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Re: [2tarasv] [2Старик]
>>Почитайте вот тут:
>> http://home.att.net/~jbaugher1/p86_25.html
>>какое количество пушечных Сейбров реально поучаствовало в корейской войне, и с кем они там воевали и подо что затачивались.
>
> На томже сайте Баугера есть отдельная сраничка про F-86D всеже стоит зайдти и почитать ;)
вы это кому предложили - мне или ув. Нечаеву?
если мне, то совершенно напрасно.
http://home.att.net/~jbaugher1/p86_6.html
Instead of using conventional cannon armament, plans were made for the armament to consist of a battery of twenty-four 2.75-inch "Mighty Mouse" Folding Fin Aircraft Rockets (FFARs), all mounted in a retractable tray in the aircraft's belly. The FFAR, developed jointly by North American and the Navy, was based on the German R4 rocket of World War II. The use of an all-rocket armament was quite innovative for the time, although a more conventional 20-mm cannon installation was studied as a standby plan.
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In February 1950, the rocket armament was selected and all plans for the standby 20-mm cannon were dropped.
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Responsibility for the electronic fire control system was assigned to the Hughes Aircraft Corporation. On November 18, 1949, the Hughes company proposed that the system be designed so that the rocket attack on the enemy aircraft would be made from a lead collision course instead of from the traditional tail pursuit curve. Hughes evolved the E-4 system for this purpose. Until the 250-kW E-4 was available, the less-capable E-3 50-kw system would be fitted to the first 37 production F-95 aircraft.
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The prototype Hughes E-3 fire-control system was received at NAA on May 26, 1950 and was installed in the second YF-95A (50-578) and tested during September. On October 17, 1950, this aircraft went to Hughes for two years of development testing.
The retractable rocket pack with twenty-four 2.75-inch "Mighty Mouse" FFAR (Folding-Fin Aircraft Rockets) rockets was fitted to 50-577 which went to Inyokern, the Navy's rocket range at China Lake, California for firing tests. The 1.75-inch rocket had a 7.55-pound explosive warhead, a velocity of 2500 feet/second at burnout, and a range of 4500 yards. First trials were carried out in February of 1951. The launcher took only a half-second to extend, and the FFARs could be fired in groups or in salvo from the launcher. The stabilizing fins were foldable, being clustered around the aft end of the rocket and snapping into position after clearing the launcher.
Если коротко, то вначале на F-86D, планировалось как ракетное, так и пушечное вооружение.
потом силовым решением оставили только ракеты (потомки R-4, кстати), Хьюз разработал радар и СУО для этих ракет.... ну и все, собственно.
ув. Геннадий Нечаев - я повторяю свой вопрос:
http://vif2ne.ru/nvk/forum/0/co/1623244.htm
Сколько выпущено перехватчиков F-86D с пушечным вооружением?