FIELD: armament.
SUBSTANCE: the guide missile has a body with a blunt nose section of low lengthening, fin unit, control surfaces located on the body nose section. The missile body is made with a additional withdrawable nose section of a lower diameter. The ratio of the diameters of the with drawable nose section and the body makes up 0.4 to 0.7. The ratio of the summary length of the main nose section and the withdrawal one and the body diameter makes up 2.0 to 3.0.
EFFECT: enhanced efficiency of missile control.
5 dwg
Title | Year | Author | Number |
---|---|---|---|
GUIDED MISSILE (MODIFICATIONS) | 2005 |
|
RU2291381C1 |
CONTROLLED PROJECTILE | 2007 |
|
RU2354922C1 |
GUIDED SHELL | 2013 |
|
RU2537357C1 |
GUIDED MISSILE | 2000 |
|
RU2166724C1 |
GUIDED PROJECTILE | 2016 |
|
RU2645322C1 |
GUIDED MISSILE | 1998 |
|
RU2135946C1 |
GUIDE PROJECTILE | 1996 |
|
RU2096735C1 |
GUIDED MISSILE | 2002 |
|
RU2233423C2 |
GUIDED PROJECTILE | 2005 |
|
RU2288436C1 |
HYPERSONIC MISSILE | 2023 |
|
RU2806859C1 |
Authors
Dates
2007-07-10—Published
2005-12-26—Filed