FIELD: rocket technology.
SUBSTANCE: invention can be used in the development of rocket heads with fluid filler. The rocket head comprises a fuse (1), an elongated warhead (2) with a liquid filler (11), an expansion chamber (12), an adapter (8) with a cover (9), a body (3), including a cylindrical (4) and animated (5) parts, central cup (7), bushing (10), transverse diaphragm (18), axial detonator (6) pressed from the front end with a threaded ring (13) by a set of flat compensators (14) and from the rear end. The diameter of the central hole of the threaded ring (13) is chosen equal to (0.75-0.95) d, where d is the diameter of the axial detonator (6). At the rear end of the central cup (7) there is a bottom cover (15) provided with an annular protrusion (16) with a cross-shaped groove (17). In the groove (17) a transverse diaphragm (18) is mounted, made of plates (19) with a length of not more than 0.97D, where D is the calibre of the head.
EFFECT: increased reliability, efficiency of operation and manufacturability of the design in conditions of mass production.
4 cl, 3 dwg
Title | Year | Author | Number |
---|---|---|---|
PROJECTILE HEAD | 2022 |
|
RU2796795C1 |
JET PROJECTILE | 2005 |
|
RU2286531C1 |
HIGH-EXPLOSIVE WARHEAD OF JET PROJECTILE | 2005 |
|
RU2291377C1 |
JET PROJECTILE WARHEAD | 2013 |
|
RU2522178C1 |
MISSILE | 2022 |
|
RU2795013C1 |
ROCKET COMMON-CHARGE WARHEAD | 2009 |
|
RU2401978C1 |
AMMUNITION | 2009 |
|
RU2402741C1 |
JET PROJECTILE HEAD | 2018 |
|
RU2700144C1 |
ROCKET WARHEAD BODY | 2023 |
|
RU2810255C1 |
HIGH-EXPLOSIVE ROCKET PROJECTILE | 1994 |
|
RU2082943C1 |
Authors
Dates
2023-07-18—Published
2022-12-07—Filed