FIELD: artillery rocket ammunition. SUBSTANCE: the jet projectile with a detachable engine has a sustainer stage, engine joined to it and staging mechanism consisting of a pusher with a disk, flange-diaphragm with a tightener and an electric primer. An orifice is made on the cylindrical section of the tightener at the end of the pusher working stroke, and the disk on the pusher is installed with radial and axial clearances. EFFECT: enhanced reliability of self- centering of the separation mechanism, and reduced force of impact at the end of the pusher working stroke. 2 dwg
Title | Year | Author | Number |
---|---|---|---|
JET PROJECTILE WITH DETACHABLE ENGINE | 1999 |
|
RU2157504C1 |
JET PROJECTILE WITH SEPARATED ENGINE | 1998 |
|
RU2133445C1 |
ROCKET | 2002 |
|
RU2202761C1 |
JET PROJECTILE | 1995 |
|
RU2105949C1 |
MISSILE WITH SEPARABLE ENGINE | 2000 |
|
RU2179702C1 |
JET PROJECTILE | 2003 |
|
RU2239782C1 |
JET PROJECTILE WITH SEPARATING ENGINE | 2000 |
|
RU2167388C1 |
JET PROJECTILE WITH SEPARATED ENGINE | 1998 |
|
RU2133444C1 |
ROCKET MISSILE | 2002 |
|
RU2235282C1 |
ROCKET ENGINE | 2006 |
|
RU2322605C1 |
Authors
Dates
2000-10-10—Published
1999-12-06—Filed