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・ S-type star
・ S-unit
・ S-VHS
・ S-24 rocket
・ S-25 (rocket)
・ S-25 Berkut
・ S-300 (missile)
・ S-300VM
・ S-310
・ S-350
・ S-400 (missile)
・ S-40503
・ S-444,823
・ S-45 (satellite)
・ S-45A
S-5 rocket
・ S-50 (Manhattan Project)
・ S-500 (missile)
・ S-520
・ S-550 (spacecraft)
・ S-63 (encryption standard)
・ S-75 Dvina
・ S-8 rocket
・ S-80-class submarine
・ S-94 (film)
・ S-acylation
・ S-Adenosyl methionine
・ S-Adenosyl-L-homocysteine
・ S-adenosyl-L-homocysteine hydrolase
・ S-adenosylhomocysteine deaminase


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S-5 rocket : ウィキペディア英語版
S-5 rocket

The S-5 (first designated ARS-57) is a rocket weapon developed by the Soviet Air Force and used by military aircraft against ground area targets. It is in service with the Russian Air Force and various export customers.
It is produced in a variety of subtypes with different warheads, including HEAT anti-armour (S-5K), high-explosive fragmentation (S-5M/MO), smoke, and incendiary rounds. Each rocket is about 1.4 meters (4 ft 6 in) long and weighs about 5 kg (11 lb), depending on warhead and fuze. Range is 3 to 4 kilometres (1.9 to 2.6 miles).
==Development==
Developed in early 1950s,〔 (C-5 ) at Ugolok Neba site〕 originally as part of the air-to-air AS-5 weapon system for the MiG-19. The rockets were tested in a series of configurations on MiG-15bis and MiG-17 jets, with the final tests complete on a MiG-17PF in January 1955. The tests revealed that the rockets did not perform as expected against aerial targets. The rocket ARS-57 was accepted into service in April 1955, with a military designation S-5.〔

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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