SPIN-STABILIZED MISSILE Russian patent published in 2002 - IPC

Abstract RU 2195627 C1

FIELD: missile armament. SUBSTANCE: spin-stabilized missile has a nose cone with a liquid filler based on petroleum products and an air cavity, device for dispersion and ignition of the filler, jet engine and a tail unit. The nose cone is made with a front cone having length (5-10)ηl, where l is the length of the nose cone, η-filler viscosity in poises, and the tailplane span makes up 2 to 4 cone lengths. EFFECT: enhanced efficiency of fire destruction, as well as enhanced accuracy and close grouping of the warheads. 2 dwg

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RU 2 195 627 C1

Authors

Akel'Ev A.I.

Belobragin B.A.

Beznosov V.I.

Denezhkin G.A.

Dmitriev B.A.

Makarovets N.A.

Malakhov A.N.

Obozov L.I.

Romanovtsev B.M.

Dates

2002-12-27Published

2001-07-19Filed