FIELD: meteorology. SUBSTANCE: head part of anti-hail rocket has hull 1 with fairing 2 in which spaces there are placed cap igniter 4, vessel 14 with liquid carbon dioxide, shutter to feed it and base 10 in which radial outlet holes 16 are drilled. The latter carry module elements 17 produced in the form of hollow cylinders with perforated side surfaces in which spaces there are located branch pipes with throttle holes at end. Other end of each branch pipe is connected through shutter to vessel 14. Module elements 17 are made fast in spaces of output holes 16 and are provided with jointing spring-loaded tabs hinged over perimeter of bottom part of module element. EFFECT: enhanced operational efficiency thanks to enlargement of useful space by reduced number of module elements, increased number of uses of head part. 3 dwg
Title | Year | Author | Number |
---|---|---|---|
NOSE CONE OF ANTI-HAIL ROCKET | 1985 |
|
SU1839964A1 |
HEAD PART OF ANTI-HAIL ROCKET | 1987 |
|
SU1468155A1 |
NOSE CONE OF ANTI-HAIL ROCKET | 1985 |
|
SU1324125A1 |
HEAD OF ANTIHAIL MISSILE | 1992 |
|
RU2045163C1 |
INERTIAL CONTROL SYSTEM OF MOVABLE OBJECT | 1989 |
|
RU2020415C1 |
HEAD PART OF ANTI-HAIL ROCKET | 1989 |
|
SU1751878A1 |
ANTIHAIL ROCKET | 1994 |
|
RU2130164C1 |
FLAME-THROWER AND PYROTECNIC FLAMING MIXTURE IGNITER | 2006 |
|
RU2326326C2 |
ANTI-HAIL ROCKET | 1989 |
|
SU1692243A1 |
GUIDED MISSILE SOLID-PROPELLANT ROCKET ENGINE, SOLID PROPELLANT IGNITER AND ROCKET ENGINE NOZZLE ASSEMBLY | 2008 |
|
RU2351788C1 |
Authors
Dates
1995-08-27—Published
1987-07-27—Filed