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