FIELD: astronautics.
SUBSTANCE: invention is intended for use in combat space equipment for aircraft engagement. Missile manipulator consists of a body, a damaging element and a pyro charge for the impact body release. Said body is coupled with housing by multiple hinged parallelogram and additional multiple hinged parallelogram. Additional hinged parallelogram is installed perpendicular to main multiple hinged parallelogram. Damaging element is connected to an additional multiple hinged parallelogram. Target sensor is in form of a pin. Piezoelectric element is secured at its end. It is configured to generate electric current at impact in order to initiate explosion of pyro charge.
EFFECT: technical result is increase of destructive ability.
1 cl, 4 dwg
Title | Year | Author | Number |
---|---|---|---|
MISSILE FOR AIRCRAFT DAMAGE | 2018 |
|
RU2710893C1 |
MISSILE FOR AIRCRAFT DAMAGE | 2019 |
|
RU2710881C1 |
PROJECTILE FOR AIRCRAFT DAMAGE | 2019 |
|
RU2735634C2 |
BALLISTIC MANIPULATOR | 2018 |
|
RU2686166C1 |
BALLISTIC MANIPULATOR | 2019 |
|
RU2720756C1 |
DYNAMIC MANIPULATOR | 2019 |
|
RU2723846C1 |
DYNAMIC MANIPULATOR | 2019 |
|
RU2721506C1 |
SWORD MANIPULATOR | 2018 |
|
RU2691172C1 |
SWORD MANIPULATOR | 2019 |
|
RU2724735C1 |
BALL MANIPULATOR | 2018 |
|
RU2691170C1 |
Authors
Dates
2019-10-23—Published
2018-01-09—Filed