FIELD: jet projectile ammunition. SUBSTANCE: jet projectile has a sustainer and an engine with a stage separation mechanism joined to it. An actuator mechanism of remote inertia action is installed in parallel with the projectile axis. The mechanism is made in the form of a non-conducting body with a fixed contact set, and a conducting body of inertia pressed by a power spring towards the stage separation mechanism. The body of inertia is made in the form of a cylinder with an inertial taper hole changing into a cylinder. The mass of the body of inertia and the force of the power spring depend on the claim and provide for generation of a signal to the stage separation mechanism at the instant of completion of operation of the projectile engine. EFFECT: enhanced reliability of engine separation from sustainer without any collision. 2 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD OF SEPARATING SUSTAINER AND DEVICE THEREFOR | 2015 |
|
RU2584401C1 |
JET PROJECTILE | 2002 |
|
RU2233424C1 |
ROCKET MISSILE | 2002 |
|
RU2235282C1 |
JET PROJECTILE WITH DETACHABLE ENGINE | 1999 |
|
RU2157504C1 |
JET PROJECTILE WITH DETACHABLE ENGINE | 1999 |
|
RU2157505C1 |
ROCKET | 2002 |
|
RU2202761C1 |
METHOD FOR LAUNCHING OF JET PROJECTILE AND COMPLEX OF FACILITIES REALIZING IT | 2000 |
|
RU2167385C1 |
ROCKET | 2003 |
|
RU2247309C1 |
MISSILE WITH SEPARABLE ENGINE | 2000 |
|
RU2179702C1 |
DEVICE OF FORCED SEPARATION OF SUSTAINER STAGE FROM BOOSTER ENGINE | 2002 |
|
RU2244898C2 |
Authors
Dates
2001-05-20—Published
2000-02-24—Filed