GUIDED ROCKET OF AERODYNAMIC SCHEME UTKA Russian patent published in 1997 - IPC

Abstract RU 2077697 C1

FIELD: design and manufacture of air-to-air, air-to-surface and surface-to-air guide rockets. SUBSTANCE: if base rocket manufactured in compliance with aerodynamic scheme Utka and incor porating module-compartment of payload with control system, mobile rudders and warhead and propulsion unit with installed wings is available there appears possibility of replacement of propulsion unit with unit of another size, mass and power which widens range of tactical usage of rocket. Invention makes it possible to keep overloads acting on rocket in flight at optimal level as well as parameters of control system in case of replacement of propulsion unit with wings. EFFECT: widened range of tactical usage of rocket. 3 dwg

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RU 2 077 697 C1

Authors

Kuz'Minskij R.D.

Davydov A.N.

Chernykh L.G.

Shusev M.I.

Makarov V.S.

Portnoj A.B.

Rejdel' A.L.

Prigoniker A.B.

Jagnjuk G.K.

Korsakov V.T.

Dates

1997-04-20Published

1981-06-02Filed