FIELD: weapons and ammunition.
SUBSTANCE: unfolding wing and a mechanism of wing unfolding are installed on different stages of a two-stage missile. The wing opens beyond its rear edge with the help of two fingers of a rotary level of an unfolding mechanism, the axis of rotation of which is installed coaxially with the axis of wing rotation.
EFFECT: reduction of rocket mass.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| UNFOLDING WING OF TWO-STAGE MISSILE | 2011 |
|
RU2482434C1 |
| UNFOLDING WING OF TWO-STAGE ROCKET | 2011 |
|
RU2478907C1 |
| MECHANISM OF AIRCRAFT OUTER WINGS UNFOLDING | 2016 |
|
RU2652035C1 |
| ELEVEN CONTROL MECHANISM | 2012 |
|
RU2505776C1 |
| ELEVON CONTROL MECHANISM | 2012 |
|
RU2518486C2 |
| DEVICE FOR TWO-STAGE ROCKET STAGES SEPARATION | 2015 |
|
RU2635812C2 |
| UNDERWATER MISSILE | 2007 |
|
RU2352894C1 |
| FOLDING AERODYNAMIC AIRCRAFT STEERING WHEEL | 2018 |
|
RU2704687C1 |
| DEPLOYABLE RUDDER OF MISSILE | 2013 |
|
RU2520812C1 |
| GLIDING SPACESHIP (VERSIONS) WITH FOLDING NOSE CONE AND METHOD OF CONTROLLING ITS DESCENT TO AIRFIELD | 2011 |
|
RU2479469C1 |
