FIELD: rocketry.
SUBSTANCE: the aerodynamic stabilizer of the salvo-fire jet projectile has a nose cone with slots and axles with springs and folding blades located on them. Wedge-shaped catches are made in the slots of the nose cone, they are expanded in the inlet section up to 1.15 to 1.7 of the thickness of the blades ear. The slot longitudinal surface is slanted at an angle of 0.3 to 1.0 deg. to the stabilizer longitudinal axis. The slot fixing surface is located at an angle of 5 to 8 deg to the slot longitudinal axis.
EFFECT: enhanced reliability of fixing of the blades in flight and enhanced range and accuracy of fire.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ROCKET STABILIZER | 2022 |
|
RU2790653C1 |
| AERODYNAMICAL STABILISER OF VOLLEY FIRE MISSILE | 2009 |
|
RU2391621C1 |
| SUPERSONIC JET SHELL FIN | 2006 |
|
RU2328695C2 |
| JET PROJECTILE WITH OPENING FINES | 1996 |
|
RU2096646C1 |
| ROCKET PROJECTILE WITH A GAS-DYNAMIC STABILIZATION SYSTEM | 2020 |
|
RU2756195C1 |
| JET PROJECTILE WITH OPENING FINS | 1996 |
|
RU2096645C1 |
| JET PROJECTILE | 2002 |
|
RU2220399C1 |
| TAIL PLANE STABILIZER OF SUPERSONIC JET PROJECTILE | 2001 |
|
RU2176066C1 |
| SUPERSONIC PROJECTILE | 2016 |
|
RU2642693C2 |
| ROTARY JET PROJECTILE | 2011 |
|
RU2451902C1 |
