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Application

2003123742/02, 2003-08-01

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Start date

2003-08-01

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Actual filing date

2003-08-01

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Published

2005-02-27

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Inventor

Alekseev V.M.Babushkin D.P.Buadze V.Sh.Gus'Kov E.I.Dan'Shin A.P.Djatlovskij M.A.Zhukov V.G.Zatrov A.A.Kondrat'Ev A.I.Konovalov E.A.Korotkova E.A.Krupyshev A.N.Lagutina I.S.Lukin N.L.Lushin V.N.Narejko V.A.Nikulin V.Ju.Pelevin Ju.A.Pechenkin M.M.Pleshcheev E.S.Sologub V.M.Sysoev M.D.Tkachev V.V.Trubenko B.I.Finogenov V.S.Fishman Eh.L.Chernousov V.G.Shakhidzhanov E.S.

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Holder

Federal'Noe Gosudarstvennoe Unitarnoe Predprijatie Nauchno-Proizvodstvennoe Predprijatie

ROLL-STABILIZED HOMING AERIAL BOMB Russian patent published in 2005 - IPC

Abstract RU 2247314 C1

FIELD: aviation materiel, in particular, homing aerial bombs.

SUBSTANCE: an equipment of global satellite navigation with a receiver of differential corrections is used in the aerial bomb as a homing system. Structurally the aerodynamic configuration of the aerial bomb is made so that a low static stability is realized in it, which allows the low-power actuators in it, which allows the low-power actuators to deflect the aerial bomb through considerable angles of attack thus providing a high maneuverability of the aerial bomb. The aerial bomb guidance system forms steep hitting trajectories, which together with the enhanced mass of the combat load, its structural parameters makes it possible to realize a high accuracy and resultant efficiency of the aerial bomb.

EFFECT: enhanced accuracy and efficiency of the aerial bomb.

4 dwg

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RU 2 247 314 C1

Authors

Alekseev V.M.

Babushkin D.P.

Buadze V.Sh.

Gus'Kov E.I.

Dan'Shin A.P.

Djatlovskij M.A.

Zhukov V.G.

Zatrov A.A.

Kondrat'Ev A.I.

Konovalov E.A.

Korotkova E.A.

Krupyshev A.N.

Lagutina I.S.

Lukin N.L.

Lushin V.N.

Narejko V.A.

Nikulin V.Ju.

Pelevin Ju.A.

Pechenkin M.M.

Pleshcheev E.S.

Sologub V.M.

Sysoev M.D.

Tkachev V.V.

Trubenko B.I.

Finogenov V.S.

Fishman Eh.L.

Chernousov V.G.

Shakhidzhanov E.S.

Dates

2005-02-27—Published

2003-08-01—Filed