FIELD: weapons and ammunition.
SUBSTANCE: guided projectile comprises wings, warhead, fuse, projectile spin angular velocity optical-fiber transducer, integrator, control hardware and poser supply. Said projectile spin angular velocity optical-fiber transducer and integrator are connected in series. Said integrator is connected to control hardware.
EFFECT: faster preparation for launching.
1 dwg
Title | Year | Author | Number |
---|---|---|---|
9M100 ANTI-AIRCRAFT GUIDED MISSILE | 2020 |
|
RU2762168C1 |
DEVICE TO LAUNCH MISSILE FROM MOBILE CARRIER | 2011 |
|
RU2465532C1 |
DEVICE TO LAUNCH ROCKET FROM MOBILE CARRIER | 2011 |
|
RU2453791C1 |
DEVICE TO LAUNCH MISSILE FROM MOBILE CARRIER | 2011 |
|
RU2465533C1 |
GUIDED PROJECTILE | 1996 |
|
RU2114383C1 |
GUIDED MISSILE | 2001 |
|
RU2199715C2 |
DEVICE TO LAUNCH ROCKET FROM MOVING CARRIER | 2011 |
|
RU2468325C1 |
CONTROLLED BULLET | 2019 |
|
RU2713831C1 |
DEVICE TO LAUNCH ROCKET FROM MOBILE CARRIER | 2011 |
|
RU2467277C1 |
DEVICE TO LAUNCH MISSILE FROM MOBILE CARRIER | 2011 |
|
RU2460029C1 |
Authors
Dates
2013-03-10—Published
2011-12-23—Filed