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2 176 373

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Application

2000115701/02, 2000-06-15

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Start date

2000-06-15

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Actual filing date

2000-06-15

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Published

2001-11-27

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Inventor

Denezhkin G.A.Makarovets N.A.Kuksenko A.F.Podchufarov V.I.Sopikov D.V.Red'Ko A.A.Zotov V.N.Nosov L.S.

(73)

Holder

Gosudarstvennoe Unitarnoe Predprijatie Nauchno-Proizvodstvennoe Predprijatie

ROCKET PROJECTILE Russian patent published in 2001 - IPC

Abstract RU 2176373 C1

FIELD: jet-propelled ammunition. SUBSTANCE: the rocket projectile has a fuse, warhead, jet engine, guide pin, igniter, nozzle unit, cover with a contact sector and the second contact with a detachable current-conducting member. The nozzle unit is provided with a threaded ring with a stop bolt projecting behind the nozzle cut. The igniter is made with a flange resting on the ring shoulder closing the nozzle inlet section and engageable through the obturator with the end of the nozzle unit. The cover is fixed on the ring, whose length of the threaded section is determined from the relation given in the description of the innovation. EFFECT: enhanced no-failure operation and safety, provision of fire from launchers with various launching systems, enhanced range of fire. 5 dwg

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RU 2 176 373 C1

Authors

Denezhkin G.A.

Makarovets N.A.

Kuksenko A.F.

Podchufarov V.I.

Sopikov D.V.

Red'Ko A.A.

Zotov V.N.

Nosov L.S.

Dates

2001-11-27—Published

2000-06-15—Filed

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