FIELD: weapons and ammunition.
SUBSTANCE: aerodynamical stabiliser consists of fairing with fixing slots and blades that fold on axes. Fairing shell in zone of fixing slots location is arranged with local bulges equal to 0.8-1.2 of blade thickness in root section. Bulges make it possible to provide for contact of blade eyes with fairing along surface equal to 0.25-0.35 of blade root section area. Thickness of end part of blade in millimetres makes 
millimetres, where Mmax is maximum flight Mach number; 
is frequency of own bending vibration of blade at maximum aerodynamical heating, Hz.
EFFECT: increased distance and accuracy of shooting due to elimination of blades and fixing slots shape variations in fairing as a result of temperature deformations and absence of vibrations and provision of low amplitude of blade bending vibration.
3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AERODYNAMIC STABILIZER OF SALVO-FIRE JET PROJECTILE | 2006 |
|
RU2313761C1 |
| ROCKET STABILIZER | 2022 |
|
RU2790653C1 |
| SUPERSONIC PROJECTILE | 2016 |
|
RU2642693C2 |
| JET PROJECTILE | 2002 |
|
RU2207495C1 |
| TAIL PLANE STABILIZER OF SUPERSONIC JET PROJECTILE | 2001 |
|
RU2176066C1 |
| SUPERSONIC JET SHELL FIN | 2006 |
|
RU2328695C2 |
| ROCKET PROJECTILE STABILIZER | 2022 |
|
RU2790655C1 |
| ROCKET PART OF JET PROJECTILE | 1999 |
|
RU2158377C1 |
| AERODYNAMIC FIN OF JET PROJECTILE | 2006 |
|
RU2301394C1 |
| ROTARY JET PROJECTILE | 2011 |
|
RU2451902C1 |
