FIELD: rocketry, applicable in small-sized complexes of various purpose.
SUBSTANCE: the guiding device for rocket launching has a launching tube and centering supports installed along the generating line of the rocket body. The front section of the tube is provided with an annular probe, having a thrust bead on the side of the tube end face. The bead projects out of the launching tube end face by no more than half the support length. The inside diameter of the bead projecting section exceeds the tube inside diameter. An elastic - deformed ring, mainly made of rubber, is clamped between the probe bead and the tube end face. The supports are feely installed on the rocket with provision of a rest of their rear section on the rocket body.
EFFECT: provided stability of the rocket aerodynamic characteristics, reduced its drag and passive weight.
3 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD OF FIRING ROUNDS AND WEAPON COMPLEX TO THIS END | 2013 |
|
RU2526725C1 |
METHOD OF FIRING ROUNDS AND WEAPON COMPLEX TO THIS END | 2013 |
|
RU2527410C1 |
ROTATING MISSILE | 2020 |
|
RU2732370C1 |
GUIDING DEVICE FOR ROCKET LAUNCHING | 1996 |
|
RU2114369C1 |
WEAPON SYSTEM | 2013 |
|
RU2535119C1 |
ANTI-HAIL ROCKET | 2019 |
|
RU2709897C1 |
SUPERSONIC ARTILLERY PROJECTILE WITH SEPARABLE WARHEAD | 2010 |
|
RU2415374C1 |
SEPARATING GUIDE DEVICE OF SUBCALIBER ROCKET PROJECTILE | 1994 |
|
RU2088889C1 |
CONTROLLED BULLET | 2012 |
|
RU2496087C1 |
TRANSPORTER-LAUNCHER CONTAINER | 2013 |
|
RU2543140C2 |
Authors
Dates
2005-03-20—Published
2003-07-08—Filed