发明名称 JET PROJECTILE
摘要 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
申请公布号 RU2233419(C2) 申请公布日期 2004.07.27
申请号 RU20020120152 申请日期 2002.07.30
申请人 发明人 MAKAROVETS N.A.;DENEZHKIN G.A.;SEMILET V.V.;OBOZOV L.I.;KASHIRKIN A.A.;PODCHUFAROV V.I.;PETURKIN D.M.;GUSHCHIN V.A.;PETROV V.L.
分类号 F42B15/00 主分类号 F42B15/00
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