Shooting homing radar SNR-75V (NATO code Fan Song E)
It is, as a cabin PV, part of the station guiding the anti-aircraft rocket complexis S-75M3 Volkhov. It is designed for the detection and tracking of air targets and guidance PLŘS on them. The cabin is transported on a wheeled chassis with detached antenna system, when a transfer to a combat position, the cabin is established on the mechanical zvedácích and the wheels are in the air. The cabin is uvodorovněna and use the crane truck is assembled antenna system, consisting of two orthogonal antennas working on the principle of dr. lewis ' scanners, supplemented by two parabolic antennas.
Lewis scanner is a device using which it is possible to rozmítat emitted beam by mechanical means, as at the time of the emergence of anti-aircraft rocket complexis S – 75 were phased antenna arrays in the realm of dreams and therefore have had designers come up with a different system of "restoring" the antenna beam without requiring mechanical movement of the entire antenna system.
For the movement of the beam after the antenna has been used a device that changed the rotational movement of the aperture emitters in the scanning space. The end of the waveguide to the rotary clutch to rotate in the "shell" that reflect radio frequency energy to the mirror antennas, and then into the space. According to the impact point of the beam is changed and the direction the beam has been vyzářen. When the "return" of the antenna sensor back to the starting point was the apertura directed inside the "shell", causing inhomogeneity in the vlnovodné route, reflection of power from the magnetron back and damage the magnetron. Why was this device mounted induction sensor, which at the time of the passage of the aperture of the emitter, equipped with a permanent magnet, the beginning of active and re-run generates pulses, which are the basis for the formation of INKB (Pulses starting and end blank). These are brought to the transmitters and ensure the shutdown of the transmitters at the time of the "re-fly" the antenna of the sensors.
The cabin rotates about a vertical axis celokruhově, the antenna system is tilted in the vertical plane in the range of -3° – 82°30'.
Radar detector is a single channel to the destination and three-channel number-guided PLŘS. Displays the real (i.e., arbitrary) number of targets in the radiation characteristics of the antennas, however, to accurately track (and thus give him the rocket) can only be on one target. It is therefore able to shell the 1 target and guide on it at the same time 3 missiles.
The antenna system consists of the following vertically and horizontally polarized antennas:
P-11V (Position H) – leafy radiation characteristics of 1.1° x 7°
P-12V (Azimuth SP) – leaf radiation characteristics of 1.1° x 7
P-13V (Azimuth LO) – the pencil beam characteristic of the 1.7°
P-14V (Position LO) – the pencil beam characteristic of the 1.7°
P-16V (RPK) - antenna transmitter control commands to the rocket
Basic tactical-technical data:
The number of simultaneously tracked targets: unlimited
The number of exactly the objectives pursued with the option of guiding the missile: 1
Number of simultaneously guided PLŘS: 1-3
Max. range: 70-150 km (according to the height and type of goal)
Max. performance: impulse 1 MW, the performance of the antenna RPK 100 kW
Frequency: 5,010-5,090 MHz and 4,910-4,990 MHz
The frequency of repetition of the broadcast: the repetition period of 544 +- 22µs = 1766 imp/s - 1915 imp/s - and the opposite. the period of the 1088+-44µs = 883 – 957 imp/s
The length of the pulse: 0,4 µs in the range of 75 km, or 0.8 µs in the range of 150 km
Table max. distance detection and tracking of one target with the characteristic features:
Type of aircraft | Height of target (km) | the Distance detection mode Narrow beam / Wide beam (km) | Distance auto tracking mode Underverse / wide beam (km) |
---|---|---|---|
Heavy bomber | 10-12 | 150 / 110 | 120 / 90 |
Medium bomber | 3 | 130 / 80 | 70 /70 |
Medium bomber | 8-12 | 130 / 90 | 80 / 80 |
Fighter | 3 | 110 / 70 | 65-55 |
Fighter | 8-14 | 120 / 75 | 70-60 |
Basic dimensions
Weight in marching / battle position (kg) | Height in marching / battle position (mm) | Width in marching / battle position (mm) | Length in marching / battle position (mm) |
---|---|---|---|
10 860 / 15 300 | 3 500 / 7 950 | 2 500 / 10 000 | 6 700 / 7 360 |
staff regulations of the ACR
Prescription Zenitnyj raketnyj kompleks S-75M, 1965
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Obrázek poskytnut laskavým svolením administrátora webu forum.presscont.eu. zdroj obrázku forum.presscont.eu
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Skenování prostoru SNR 75:
Režim úzký paprsek, používal se při vyhledání a zachycení cíle na dálce větší než 70 km, u PLRK S-75M3 bylo též možno v něm vést střelbu. Diagram vyzařování v ÚP:
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Režim široký paprsek, používal se při vyhledání a zachycení cíle na dálce 70 km a menší. Základní režim pro střelbu na cíle ve výškách menších než 5 km. Diagram vyzařování v ŠP:
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Režim ozáření (podsvět), základní režim pro střelbu pro cíle na větších výškách než 5 km. Obě antény ÚP soustředily svoje vyzařovací charakteristiky do jednoho bodu, přičemž příjem signálu zabezpečovaly antény ŠP. Výhodné zejména při střelbě za rušení, pr
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Režim IPR (Impulsně selektivní režim – bohužel na správný ruský výraz jsme si nevzpomněli), používal se při střelbě na cíle, u nichž hrozilo použití protiradiolokačních střel. Příznakem bylo, že cíl otočil na přílet a letěl s kurzovým parametrem blízkým 0