FIELD: rocket technology.
SUBSTANCE: invention relates to rocket technology, namely to the rocket part of a jet-propelled projectile. The rocket part of a jet-propelled projectile contains a housing, a stabilizer block and a sleeve. On the outer surface of the housing in the area bounded by the sleeve and the threaded connection to the stabilizer block, a turbulator is made containing a cylindrical surface with a conical transition section from the cylindrical surface to the outer surface of the housing. The diameter of the cylindrical surface is (0.95…0.99)D. The length of the turbulator is (0.02…0.15)D. The taper angle of the conical sections is (30…70)°, where D is the caliber of the rocket part.
EFFECT: increase in the reliability of the functioning of the rocket part and eliminating the misalignment of the body of the rocket part with the stabilizer block.
1 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| JET PROJECTILE ROCKET SECTION | 2013 |
|
RU2537189C1 |
| ROCKET PART OF ROCKET MISSILE | 2016 |
|
RU2631882C1 |
| ROCKET MISSILE | 2016 |
|
RU2631727C1 |
| SOLID-PROPELLANT ROCKET ENGINE BODY | 2010 |
|
RU2447310C1 |
| JET PROJECTILE | 2002 |
|
RU2207495C1 |
| MISSILE | 2016 |
|
RU2623373C1 |
| BODY OF SOLID-PROPELLANT ROCKET ENGINE | 2006 |
|
RU2317434C1 |
| JET PROJECTILE WITH SEPARATED ENGINE | 1998 |
|
RU2133444C1 |
| ROCKET PART OF MISSILE FIRED FROM TUBULAR GUIDE | 2023 |
|
RU2808695C1 |
| ROCKET MISSILE | 2002 |
|
RU2235281C2 |
