FIELD: rocketry. SUBSTANCE: jet projectile has a jet engine, made in the length within 1.8-3 of the caliber before the stabilizing fin with reduction, and its diameter makes up 0.7-0.8 of the projectile caliber. The stabilizing fin fairing has a diameter of 0.9-1.0 of the caliber and is provided with a tapered adapter connecting it to the jet engine. The adapter length equals 0.3-0.6 of the caliber. The projectile nose is connected to the jet engine through a tapered flare, having a length of 0.5-1.0 of the projectile caliber, and the blade span of the stabilizing fin corresponds to the relation given in the claim. EFFECT: enhanced aerodynamic power of the stabilizing fin, enhanced relative coordinate of the center of gravity, and as result, enhanced flight stability and reliability of projectile functioning. 1 dwg
| Title | Year | Author | Number | 
|---|---|---|---|
| JET PROJECTILE | 2002 | 
 | RU2207495C1 | 
| SPIN-STABILIZED SUPERSONIC MISSILE | 2000 | 
 | RU2166178C1 | 
| ROCKET PROJECTILE | 1999 | 
 | RU2151367C1 | 
| DETACHABLE NOSE CONE OF JET PROJECTILE | 2001 | 
 | RU2176375C1 | 
| TAIL PLANE STABILIZER OF SUPERSONIC JET PROJECTILE | 2001 | 
 | RU2176066C1 | 
| SALVO-FIRE JET PROJECTILE ELONGATED BY MORE THAN 20 CALIBERS | 1998 | 
 | RU2150081C1 | 
| ROCKET PROJECTILE STABILIZER | 2022 | 
 | RU2790655C1 | 
| ROTARY JET PROJECTILE | 2011 | 
 | RU2451902C1 | 
| SUPERSONIC JET PROJECTILE | 2005 | 
 | RU2294523C1 | 
| SUPERSONIC PROJECTILE | 2016 | 
 | RU2642693C2 | 
Authors
Dates
2001-04-27—Published
2000-06-26—Filed