FIELD: weapon.
SUBSTANCE: invention relates to missile munitions. The method of guided missile launch includes targeting of the missile, increase of its length due to impulse boost and further inertial shift of its head and firing the missile. The head of the missile is made from telescopically shifted members. The length of the missile is shifted due to their sequential shifting, breaking and fixation with decrease of the total weight.
EFFECT: decrease of pre-launch indignations effected the missile and launcher with providing higher length of the missile.
4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| GUIDED MISSILE | 2008 |
|
RU2370725C1 |
| GUIDED MISSILE | 2007 |
|
RU2351886C1 |
| GUIDED MISSILE | 2008 |
|
RU2370726C1 |
| GUIDED SHELL | 2007 |
|
RU2351887C1 |
| GUIDED MISSILE | 2002 |
|
RU2222768C2 |
| GUIDED MISSILE | 1994 |
|
RU2084809C1 |
| GUIDED MISSLE | 2007 |
|
RU2358229C2 |
| GUIDED PROJECTILE | 2009 |
|
RU2406063C1 |
| GUIDED MISSILE | 2001 |
|
RU2218546C2 |
| MULTIMISSION GUIDED MISSILE IN LAUNCHING PACK | 2004 |
|
RU2277693C1 |
