FIELD: war equipment. SUBSTANCE: missile has a nose fairing and fuze contact device. Secured on the front end of the nose fairing is a nozzle with a conical cutting part made perpendicularly to the MISSILE longitudinal axis. At an approach of MISSILE to a metal screen at different angles of impact the nozzle pierces the screen. Any damage to the nose fairing by the screen and destruction of the fuze contact device are excluded. EFFECT: enhanced reliability. 1 dwg
Title | Year | Author | Number |
---|---|---|---|
GUIDED MISSILE | 1997 |
|
RU2124695C1 |
GUIDED MISSILE WARHEAD | 1994 |
|
RU2072504C1 |
CONTACT DEVICE | 2001 |
|
RU2206061C2 |
GUIDED MISSILE CONTROL ACTUATOR | 1993 |
|
RU2072506C1 |
SHELL | 1997 |
|
RU2125228C1 |
GUIDED MISSILE CONTROL ACTUATOR UNIT | 1996 |
|
RU2092783C1 |
GUIDED MISSILE | 1995 |
|
RU2088890C1 |
GUIDED MISSILE | 1998 |
|
RU2127417C1 |
GUIDED MISSILE | 1996 |
|
RU2101664C1 |
GUIDED MISSILE NOSE CONE | 1995 |
|
RU2089834C1 |
Authors
Dates
1996-09-20—Published
1993-06-22—Filed