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・ 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
・ S-adenosylhomocysteine hydrolase
・ S-Adenosylmethioninamine
・ S-adenosylmethionine synthetase enzyme
・ S-algol
・ S-alkyl-L-cysteine sulfoxide lyase
・ S-alkylcysteine lyase
・ S-Allyl cysteine


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S-8 rocket : ウィキペディア英語版
S-8 rocket

The S-8 is a rocket weapon developed by the Soviet Air Force for use by military aircraft. It remains in service with the Russian Air Force and various export customers.
Developed in the 1970s, the S-8 is an 80 mm (3.1 in) rocket used by fighter bombers and helicopters. The system entered service in 1984 and is produced in a variety of subtypes with different warheads, including HEAT anti-armor, high-explosive fragmentation, smoke, and incendiary, as well as the specialized S-8BM runway-destroying munition and the S-8DM fuel-air explosive variants. Each rocket is between 1.5 meters (4 ft 11 in) and 1.7 meters (5 ft 7 in) long and weighs between 11.3 kg (25 lb) and 15.2 kg (33.5 lb), depending on warhead and fuse. Range is 2 to 4 kilometers (1.3 to 2.6 mi).
The S-8 is generally carried in the B series of rocket pods, carrying either seven or 20 rockets.
==Rocket specifications==

An upgraded version, S-8OFP, has a length of 1.428 m, a weight of less than 17 kg, and a range of 6 km.

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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