FIELD: rocketry, in particular, jet projectiles of salvo-fire systems.
SUBSTANCE: the jet projectile has a hose, powder charge of solid propellant, thin-walled body of the rocket unit, nozzle and an aerodynamic tailplane. The aerodynamic tailplane and the nozzle are made as a monoblock unit connected to the body of the rocket unit. The mass of the monoblock unit equals 0.7 to 0.9 of the mass of the body of the rocket unit. The nose mass makes up 1.1 to 1.5 of the total mass of the body of the rocket unit and monoblock unit. The nose length makes up at least 0.4 of the length of the body of the rocket unit.
EFFECT: enhanced projectile range.
1 dwg
Title | Year | Author | Number |
---|---|---|---|
JET PROJECTILE | 2002 |
|
RU2207495C1 |
MISSILE UNIT OF JET PROJECTILE | 2003 |
|
RU2255298C1 |
SUPERSONIC JET MISSILE | 2007 |
|
RU2357193C1 |
ROCKET PROJECTILE LAUNCHED FROM LAUNCHING TUBE | 1997 |
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ROTARY JET PROJECTILE | 2011 |
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RU2451902C1 |
ROCKET PART OF JET PROJECTILE | 1999 |
|
RU2158377C1 |
ROCKET | 1998 |
|
RU2150080C1 |
SUPERSONIC JET PROJECTILE | 2001 |
|
RU2180093C1 |
ROCKET PROJECTILE | 1999 |
|
RU2151367C1 |
SPIN-STABILIZED SUPERSONIC MISSILE | 2000 |
|
RU2166178C1 |
Authors
Dates
2004-07-27—Published
2002-07-30—Filed