BICALIBER GUIDED MISSILE Russian patent published in 1998 - IPC

Abstract RU 2114382 C1

FIELD: small-sized rocket projectiles. SUBSTANCE: releasable booster engine is telescope-joined to the tip section of the sustainer stage. The tip section of the sustainer stage and location for it in the booster engine are made cylindrical, stepped with lowering to the rear end. The booster engine in its front section is furnished with a destabilizer and attenuators in the form of through slots. EFFECT: reduced disturbances of sustainer stage at staging. 2 cl, 2 dwg

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RU 2 114 382 C1

Authors

Zhukov V.P.

Rasskazov A.V.

Khripunov L.A.

Kuznetsov V.M.

Dates

1998-06-27—Published

1996-02-27—Filed