ANTIAIRCRAFT GUIDED MISSILE
申请公布号:RU2133446(C1)
申请号:RU19980111140
申请日期:1998.06.09
申请公布日期:1999.07.20
发明人:KUZNETSOV V.M.;EHNTIN A.P.;FERULENKOV A.V.;GORBUNOV B.A.;TRESHCHEV I.L.;MAKHONIN V.V.
分类号:F42B15/10;(IPC1-7):F42B15/10
主分类号:F42B15/10
摘要:FIELD: rocketry. SUBSTANCE: missile has interconnected zero and sustainer stages. The sustainer stage case is made in the form of a thin-walled envelope connected to the nose fairing. The functional units and live ammunition interconnected in axial direction are located inside the envelope. Part of the envelope around the live ammunition is made as an additional mass of warhead hitting components. EFFECT: enhanced stiffness of sustainer stage airframe, reduced overall dimensions and mass, improved aeroballistic characteristics of missile. 2 cl, 2 dwg
KRYSS-BUNDETE HYDROGELER OG DERES ANVENDELSE SOM SAARFORBINDINGER.
FIBEROPTISK RADARLEDET MISSILSYSTEM.
ELECTRICAL MOTOR WITH IMPROVED TACHOMETER GENERATOR
FREMGANGSMAATE VED FREMSTILLING AV HUMAN PROUROKINASE.
PROCEDIMIENTO MICROBIOLOGICO PARA PREPARAR HETEROPOLISACARIDOS A PARTIR DE XANTHOMONAS CAMPESTRIS
VERFAHREN ZUR NACHBEHANDLUNG EINES BETONFORMKOERPERS.
EINRICHTUNG UND VERFAHREN ZUR FEINSTBEARBEITUNG VON OBERFLAECHEN.
NASENHEILMITTEL MIT VITAMIN B12.
HYBRID PLASTIC FILLING MATERIAL
SHOGAIYUNITSUTOKIRIHANASHIKENSHUTSUHOSHIKI
FOCUS CONTROL SIGNAL DETECTING SYSTEM IN OPTICAL DISK DEVICE