FIELD: armament.
SUBSTANCE: the radio-controlled missile has a separating engine, sustainer stage with the control equipment connected to the antenna device in the form of a sustainer antenna positioned on the rear end face of the sustainer stage and two start antennas. The aft part of the sustainer stage with the sustainer antenna is positioned in the cavity made on the front end face of the engine. The start antennas are positioned on the lateral surface of the sustainer stage. The antenna device is provided with a waveguide switch having outgoing arms, one of which is connected to the input of the control equipment, and the others - to the antennas provided with movable dampers.
EFFECT: enhanced reliability of the radio-controlled missile and reduced signal distortion.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| RADIO-CONTROLLED ANTI-AIRCRAFT MISSILE | 2001 |
|
RU2184343C1 |
| RADIO-CONTROLLED MISSILE | 2006 |
|
RU2303234C1 |
| RADIO-CONTROLLED MISSILE | 2003 |
|
RU2255297C1 |
| RADIO-CONTROLLED ANTI-AIRCRAFT MISSILE | 2000 |
|
RU2189003C2 |
| RADIO-CONTROLLED PROJECTILE | 2023 |
|
RU2825229C1 |
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|
RU2373486C1 |
| MISSILE | 2011 |
|
RU2460965C1 |
| MISSILE | 2005 |
|
RU2284457C1 |
| ROCKET | 2016 |
|
RU2613391C1 |
| RADIO-CONTROLLED MISSILE | 2019 |
|
RU2710340C1 |
