FIELD: armament, in particular, guided missiles.
SUBSTANCE: the guided missile has a body with a warhead and a casing positioned in succession in it, the control equipment units are located in the casing. A flange with a stop in the end face of the warhead and the casing is installed between the warhead and the casing. Annular bosses uniformly distributed in its longitudinal axis and engageable with the inner surface of the body provided with a stop in the bottom section are made on the outer surface of the casing. The warhead is installed in the body with compression the side of the front end face.
EFFECT: enhanced initial velocity and enhanced allowable launching g-loads.
2 dwg
Title | Year | Author | Number |
---|---|---|---|
GUIDED PROJECTILE | 2005 |
|
RU2288438C1 |
GUIDED PROJECTILE | 2008 |
|
RU2380649C1 |
GUIDED MISSILE | 2003 |
|
RU2248516C1 |
CONTROLLED PROJECTILE | 2010 |
|
RU2442102C1 |
SHELL AND METHOD FOR ASSEMBLAGE OF SHELL | 1999 |
|
RU2157502C1 |
CONTROL COMPARTMENT AND AUTOPILOT UNIT OF HOMING ARTILLERY PROJECTILE | 2004 |
|
RU2265789C1 |
GUIDED MISSILE CONTROL BAY | 2000 |
|
RU2176377C2 |
METHOD FOR PROTECTION OF SENSING ELEMENTS OF GUIDED MISSILE ROLL GYROSCOPE FROM ACTION OF LAUNCH G-LOADS, GUIDED MISSILE FOR ITS REALIZATION AND METHOD FOR ITS ASSEMBLY | 2006 |
|
RU2308671C1 |
GUIDED PROJECTILE | 2016 |
|
RU2633716C1 |
METHOD FOR STRENGTH TEST OF AUTOPILOT UNIT OF GUIDED MISSILE WITH HOMING HEAD AND DEVICE FOR ITS REALIZATION | 2000 |
|
RU2173829C1 |
Authors
Dates
2005-01-20—Published
2003-11-17—Filed