FIELD: rocketry. SUBSTANCE: guided missile has the leading shaped charge and the main warhead with safety-and- actuating mechanisms, as well as the control actuator unit with coils of the polarized control electromagnet, and coil of two-wire communication line. The communication line coil is connected to the beginnings of the coils of the control electromagnet of the control actuator unit, and the ends of these coils are combined by a jumper and parallel- connected to the safety-and actuating mechanisms of the leasing shaped charge and the main warhead. EFFECT: enhanced reliability of the safety-and-actuating mechanisms and the missile on the whole. 2 dwg
Title | Year | Author | Number |
---|---|---|---|
GUIDED MISSILE NOSE CONE | 1996 |
|
RU2100767C1 |
GUIDED MISSILE | 1996 |
|
RU2101664C1 |
GUIDED PROJECTILE | 1996 |
|
RU2095738C1 |
METHOD FOR PROVISION OF ELECTRIC POWER SUPPLY FOR AIRBORNE EQUIPMENT OF GUIDED MISSILE AND GUIDED MISSILE IN TRANSPORT-LAUNCHING PACK FOR ITS REALIZATION | 2002 |
|
RU2233420C2 |
GUIDED PROJECTILE | 1998 |
|
RU2150082C1 |
GUIDED MISSILE | 1995 |
|
RU2092778C1 |
GUIDED MISSILE | 1998 |
|
RU2125230C1 |
GUIDED MISSILE | 1993 |
|
RU2056619C1 |
GUIDED MISSILE NOSE CONE | 1995 |
|
RU2089834C1 |
GUIDED MISSILE | 1992 |
|
RU2046281C1 |
Authors
Dates
1999-03-10—Published
1998-02-16—Filed