SOV - SA-75 Dvina / S-75 Děsna / S-75M Volchov / S-75M Volha [kód NATO: SA-2 Guideline]
přehled verzí
SA-75 Dvina
S-75 Děsna
S-75M Volkhov
S-75 Volga
The naval version of the:
M-2 Volkhov-M
Code table of the NATO
System | Rocket (factory designation) | Rocket (military designation) | Code NATO | Launchers | Shooting homing radar – the original name | Shooting homing radar – the name of the NATO code |
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SA-75 Dvina | -750 | 1D | SA-2a Guideline | SM-63 | RSNA-75 | Fan Song And |
SA-75M Dvina | IN-750V | 11D | SA-2b Guideline Mod 1 | SM-63-I | RSNA-75M | Fan Song B |
S-75 Děsna | IN-750VN | 13D | SA-2c Guideline Mod 2 | SM-63-I | RSN-75 | Fan Song C |
S-75D Děsna | V-750VN/V-755 | 13D/20D | Without the code | SM-63-IIA | RSN-75 | Fan Song C |
S-75M Volkhov | -755 | 20D | SA-2d Guideline Mod. 3 | SM-90 | RSN-75V | Fan Song E |
S-75M Volkhov | -760 | 15D | SA-2e Guideline Mod 4 | SM-90 | RSN-75V | Fan Song E |
S-75M2 | -759 | 5Ja23 | SA-2f Guideline Mod 5 | SM-90 | RSN-75V2 | Fan Song F* |
M-2 Volkhov-M | -753 | 13DM | SA-N-2 Guideline | SM-64 | | |
* - West thought, that the terms of the S-75M2 Volkhov with a rocket 5Ja23. In fact, however, it was the SA-75M Dvina and RSNA-75M, as supplemented by the optical channel of the PA-00. See the relevantarticle
Version WITH-75M1-4 Volkhov do not already have their own codes and, moreover, the West had a bit of confusion in what is actually different versions differed.
Export versionS-75 Volga did not own the code..
BN - conventional fighting.
JaBN - nuclear combat load
And if someone counts, so there is really 36.
Type Type | Rocket Missile | Factory index Factory Index | Description Description |
---|---|---|---|
normal normal | -750 | 1D | length of shooting 7 - 29 km, the height of the firing 3000 - 23000 m Photograph, firing range 7 - 29 km, photograph, firing altitude 3000 - 23000 m |
normal normal | IN-750V | 11D | length of shooting 7 - 29 km, the height of the firing 3000 - 25000 m, BN 190 kg, the average of the 500/654 mm, weight 2163 kg, the length of 10726 mm Photograph, firing range 7 - 29 km, photograph, firing altitude 3000 - 25000 m, Weight 2163 kg, Lenght 10726 mm, Warhead weight of 190 kg, Diameter 500 / 654 mm |
normal normal | IN-750VK | 11D | upgraded rocket Modernized missile |
normal normal | IN-750VM | 11DM | rocket fire on the jammer Missile for the photograph, firing it aircraft - jammer |
normal normal | IN-750VM | 11DU | upgraded rocket Modernized missile |
normal normal | IN-750VM | 11DA | upgraded rocket Modernized missile |
normal normal | IN-750M | 20TD | I don't have more information Have not specific information |
normal normal | IN-750SM | - | I don't have more information Have not specific information |
normal normal | IN-750VN | 13D | length of shooting 7 - 29/34 km, the height of shooting 3 - 25/27 km, the length of 10841 mm Photograph, firing range 7 - 29/34 km, photograph, firing altitude 3000 - 25000/27000 m, Lenght 10841 mm |
normal normal | - | 13DA | the rocket with the new BN 191 kg Missile with new warhed weight 191 kg |
normal normal | IN-750AK | - | I don't have a closer inforamce Have not specific information |
normal normal | -753 | 13DM | rocket for maritime PLRK M-2 Volkhov-M (SA-N-2 Guidelaine) Missile from a naval SAM system M-2 Volkhov-M (SA-N-2 Guideline) |
normal normal | -755 | 20D | length of shooting 7 - 43 km, the height of shooting 3 - 30 km, the weight of 2390 - 2396 kg, BN 196 kg length mm 10778 Photograph, firing range 7 - 43 km, photograph, firing altitude 3000 - 30000 m, Weight 2360 - 2396 kg, Lenght 10778 mm, Warhead weight 196 kg |
normal normal | -755 | 20DP | the rocket with the possibility of shooting on passive stretch, the length of the firing 7-45 km to the active, 56 km to the passive section, the height of the firing 300 - 30000 (35000) m Missile for the photograph, firing on passive flight-line, photograph, firing range 7 - 45 km active, 56 km passive, photograph, firing altitude 300 - 30000 (35000) m |
normal normal | -755 | 20DA | rockets with expired service life, and the redesigned 20DS Missile with expired lifetime period and remodelled it 20DS |
normal normal | IN-755OV | 20DO | rocket for sampling air in the implementation of the tests (with an additional rocket engine solid fuel) Missile for the taking of samples of air at tests |
normal normal | IN-755U | 20DS | rocket with a selective block of the for shooting at altitudes of less than 200 m Missile with selectvive block for photograph, firing to target in a low altitude (under 200 m), photograph, firing altitude 100 - 30000 / 35000 m |
normal normal | IN-755U | 20DSU | rocket with a selective block of the for shooting at altitudes of less than 200 m, and reduced time pre-launch preparations Missile with selectvive block for photograph, firing to target in a low altitude (under 200 m) and shortening time preparation the missile to fire, photograph, firing altitude 100 - 30000 / 35000 m |
normal normal | IN-755U | 20DU | the rocket had shortened the period of pre-launch preparations Missile with shortening time preparation the missile to fire |
normal normal | -759 | 5Ja23 (5V23) | length of shooting 6 - 56 (60/ 66 km), the height of the shooting of 0.1 - 30 km, the weight of 2406 kg, the length of 10910 (10806) mm, BN 197 - 201 kg Photograph, firing range 6 - 56 (or 60 or 66 km), photograph, firing altitude 100 - 30000 / 35000 m, Weight 2406 kg, Lenght 10806 mm, Warhead weight 197 - 201 kg |
normal normal | -760 | 15D | rocket without destabilizing pads, JaBN 10 kt Missile with a nuclear warhead 10 kt |
normal normal | IN-760V | 5V29 | rocket with JaBN Missile with a nuclear warhead |
development development | IN-750IR | - | rocket with a pulse radiozapalovačem Missile with a pulse radiofuse |
development development | IN-750N | - | rocket wavelength range of N, the test The Test of the missile, the N-band |
development development | IN-750P | - | experimental rocket with a revolving wing Experimental missile - with wings rotate |
development development | -751 | KM | rocket - flying laboratory on the basis of uncontrolled rockets "025" Experimental missile - flying test bed |
development development | -752 | - | variant of the missile with the location of the starting position of the rocket engines on the sides Experimental missile - boosters at the sides |
development development | -754 | - | variant of the missile with semi-active radar homing warhead Experimental missile - with semi-active homing head |
development development | -757 | 17D | test rocket with náporovým rocket motor Experimental Missile - with scramjet |
development development | - | 18D | test rocket with náporovým rocket motor Experimental Missile - with scramjet |
development development | In-757Kr (3M10) | - | variant of the missile-757 for PLRK 2K11 Krug (SA-4 Ganef) Experimental Missile - version for2K11 Krug (SA-4 Ganef) |
development development | -758 (5 JaGG) | 22D | test the three-stage rocket, the weight of 3200 km, the speed of 4.8 M (1560 m/s, 5760 km/h) Experimental Missile - three-stage missile, Weirht 3200 kg, a Speed Of 4.8 M (= 1560 m/s = 5760 km/h) |
target target | Korshun | - | target rocket Target missile |
target target | RM-75MV | - | target rocket for small height Target missile - for low altitude |
target target | RM-75V | - | target rocket for high altitude Target missile - for high altitude |
target target | Sinica-23 | 5Ja23 | target rocket Target missile |
target target | RM-75 | Armavir | target rocket Target missile |
Source information:
Own notes, 20 years, I have worked with all the PLRK and the ASV of NAD in the CSLA (71.plrb).
If something you don't understand, so get in touch..
The following lines I am writing entirely from memory, if I think of further clarification, I will add it.
Anti-aircraft missile complexes (PLRK) S-75 Volkhov, which were used on the territory of the CZECHOSLOVAK socialist republic (Czech and Slovak federative republic, CZECH republic) were in the following modifications:
S-75V, S-75M, S-75M* and S-75M3.
On the territory of the CZECH republic was included in the assembly 71.plrb 8 PLRK (defense of Prague and central Bohemia) in the case 1. to 8.plro and 185.plrp 5 PLRK (defense of the state border with GERMANY).
S-75V – the basic version of PLRK S-75 Volkhov
S-75M – compared with the s-75V improved ways of tracking of the objective, a little bit of a different setting of the system the calculation of the commands for the rockets
S-75M* - complemented by the visual channel (used a TV camera, which enabled the retrieval, monitoring and postřelování goals in the optical regime using the method of "three points" without radiating electromagnetic energy
S-75M3 – improved ways of monitoring objectives, in aparaturách more used semiconductors, new power 2x100 kW
PLRK S-75 Volkhov all the modifications consisted of:
Radiotechnické battery, which was formed by the terminus of the trans-SNR-75 in the assembly of cabins:
UV (control cabin) includes
- the system of the officer's guide (finding your target, the transmission of the objective to capture, the choice of methods, redesigning, firing rockets etc)
- systems operators azimuth (β - beta), the positioning of the angle (ε - epsilon) and the distance (D)
- training system rockets
- the workplace of the commander of the (profitable indicator circular looms from the RLD P-12, somewhere P-18)
- the imitative apparatus for training
AV (instrument enclosure) included
- system (koordinaty – calculation of the coordinates of the target and the rockets + mezifrekvenční and the low frequency part of the receiver)
- system SVK (sistěma vyrabotky squads – the calculation of the commands for the missile)
- the system of RPK (radioperedatčik kommand – transmitter commands on board the rocket)
- system SDC (selekcija dvižajuščich the whole – selection of moving targets = protection from passive interference)
PV (broadcast cabin) includes
- the antenna of a wide beam for azimuth and the orientation angle (leafy characteristics of emission, the thickness of the sheet of 1.1° , a width of 7°)
- antenna narrow beam for azimuth and the orientation angle (tužková characteristics of emission, an average of 1.7°)
- the antenna of the transmitter commands
- in modification of the M* and M3 TV camera
- the transmitter for the azimuth and the orientation angle (the output level is executed magnetronem, the length of the waves of approximately 6 cm, pulse performance in each plane of the 1 MW)
- the high-frequency part of the receiver for the azimuth and the orientation angle (at the entry of used tubes with the progressive wave)
RV / RKU (grid cabin) includes
- managing the counters for the distribution of electric energy to power all of the cabins and launcher 50 Hz and 400 Hz
- voltage converter 50 Hz to 400 Hz (400 Hz distribution systems were used for anodová voltage because of the reduced ripple after rectification)
- managing the counters for the operation of the power generators
- generator of 30 kW (only on the power PLRK in the off state for lighting, fans etc)
EDS (eletrocentrály)
- 3 power of 100 kW (u S-75V, M and M*)
- 2 power 2x100 kW (u S-75M3)
Furthermore, there was
- radar range finder, P-12 or P-18
- coupler cabin 5F20 to connect to the automatic system of command for the ASV Seněž, 5Ch56 for Asurk-1ME and or 5F24 for Vector
- the cab and the antenna of the system of recognition of the own – foreign (ZEF)
- station radioreléového conjunction with the supervisor for the communication and transmission of data from the ASV 5Ja62 (two directions) or 5Ja63 (in three directions) for ASV Seněž and Vector or R-404 for Asurk
The fire of the battery:
- Launchers SM90 – 6pcs
- Anti-aircraft missile (plřs) 20DP, 20DSU or 5Ja23 – the numbers and types according to the dislocation of the plro, as a rule, not less than 12 and not more than 18
- To launch the devices to be maintained 5 plřs, the sixth was dedicated to the training of
- Přepravník plřs PR-11B – numbers once again by the dislocation of the plro, as a rule, not less than 8 and not more than 12.
1. Pitot tube: u Dviny is vysouvala, therefore, should be on the cutting edge of the stronger short "nose", u Volchovu to download the cover, therefore, on the cutting edge of the thinner and longer tube.
2. The antenna of the receiver radiozapalovače: have been placed in front of the wings 2.grades for both types. for Dviny but they were recessed into the hull of the rocket, whereas the Volchovu protrude in the housings above the surface.
3. Stabilizers 1.grades: u Dviny were on the top and bottom of the stabilizer aerodynamic correction of the surface (when viewed from the rear), for Volchova nothing, only the smooth surface.
The differences is, of course, much more, these are but the most striking ones, which will help for the immediate assignment of the rocket to the complex. Therefore, it would be possible to fix some of the above minor inaccuracies..
Modernization according to the program of the Volga-2A predpokladala vymenu several analogovych system for cislicovou apparatus. It would extensively vylepsilo technical parameters of a system.
Unfortunately, more information about this modification I already nenasel. Probably from the other modernisation dropped, because in a's time have PLRK S-75 tri fundamental shortcomings:
1) due to the cili is jednokanalovy.
2) is mobile, but casy on svinuti/rozvinuti are relatively long (from own practice of vim, of we it the fastest catch in about 1 hr 20 min / 1 hr 30 min, but it was zabiracka and after rozvinuti is nesmela occur none fundamental node.
3) problem with udrzbou rockets - 2.[mel kapalinovy raketovy the engine and the system skladovani etc ma far into the is no modernich solutions with ulozenim rockets in hermetizovanych containers, when not may not be sahnout 10 or even vice years.
In the present is the S-75 fully replaced by PLRK S-300 to all of the modification..
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specimen of the Warsaw museum.
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vlastní foto
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Exponát VMH Piešťany.
I think on a carrier is the Dvina and another picture of the Volkhov and S-200.
Dvina,the air museum Kbely, own photo.
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Own photo.
The difference between the missile V-755 (20D) and V-759 (5Ja23)
- The 20D has 4 receiving antenna radiozapalovače placed in the axes of the wings (one pair for an angle of 78°, the second for 87°)
- 5Ja23 has only one pair of antennas located in the horizontal axis of the rocket just behind the destabilizačními the lands of the..
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V-759 / 5Ja23
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V755 / 20DSU
Question the first: How it looks OR the inside?
Inside the shells OR are primarily actuators, i.e. motors, amplidynes, different blocks, etc. Ramp SM-90 I never from the inside shot, and at Dvin, I didn't do. One ramp SM-63 while she stayed with us in the barracks, but that has all the internal equipment removed.
Question the second: What is the difference between SM-90 complex of the Volkhov and SM-63 complex Dvina?
I repeat – with Dvinou I've never worked, so only two photos. The differences is to see enough, but the exact dimensions or weight of SM-63 don't know. Note also the differences between the rockets 11D and 20D.
Question the third: Is it possible to build a diorama, where the Dvina and near the team of the Green berets, which picks up the helicopter?
According to me no. Battle stations looks as follows. In the middle is a guidance locator and cabin and in a circle around the are up OR. Distance OR from the NRL is normally 100 m, but in Vietnam, these were the distance shortened to only 35 m.
Anti-aircraft rocket complexis were the most secretive and most guarded of the north vietnamese resources. Their defense was therefore paid great attention.
Around the anti-aircraft rocket complexis was set up circular defence against ground assault, but the main defense was from air danger. Each section had to defend themselves singled out three batteries malorážního PL artillery (caliber 37 and 57 mm) and three to four platoons PL machine guns (ZPU-2 or ZPU-4 caliber 14.5 mm). These PL funds were deployed in an irregular circle around the section, while the cannons were placed in education. 1,5 – 2 km and machine guns 200 – 700 m.
I believe that even stupid Americans

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Jinak zdravím bývalé kolegy, kteří sem nepochybně přispívají. Rád vzpomínám na časy naší služby v hotovostním systému PVOS.
The information is contained on the line, which is in my post indicated (this is a link to the NPO Almaz, which With-75ky developed and also produced).
Although it is a certain contradiction (mainly time) between the information on the S-75 on the website Almazu and www.pvo.guns.ru, but they have one thing in common - u S-75M4 was used in the new design of the antennas of the narrow beam.
I have been on the rifle a total of 14x (last in 1989) and on the S-75M4 the speech was not.
Personally, I gravitated to as a correct indication of the type of S-75M4 rather by the manufacturer (i.e. Almaz).
Get the name of the line on the page Almazu linked with the name of the academician And.And.Raspletina, who was the chief designer of PLRK S-25 Berkut and also the S-75 ...
By the way, of which the Volga you were shooting?
Franta.
- in the picture 100_7185.jpg is rocket 11D or 13D (see few details, that's why I can't accurately determine) on the freighter PR-11A with the truck ZiL-157, include anti-aircraft rocket complexis SA-75M Dvina by the way, when was this spring in Israel the Day of air defence, so there hasn't been and this place was empty.
- in the picture 100_7182.jpg it is left to the missile 5V28 on OR 5P72 from anti-aircraft rocket complexis S-200VE Vega, the right is the rocket 5Ja23 to the OR SM-63-II *)
- in the picture Frame 104.jpg is rocket 1D to the OR SM-63-I
*) originally, this sentence continued "...and it belongs to the anti-aircraft rocket complexis S-75M* or higher".
Due to the fact that today I know why is this combination in Israel realized, here is the explanation: in the republic of simply OR SM-90 didn't get, so they used that OR they have managed to get hold of..
Quote - Franta02 :
To photos from karaca let me clarify:
- in the picture 100_7185.jpg is rocket 11D or 13D (see few details, that's why I can't accurately determine) on the freighter PR-11A with the truck ZiL-157, include anti-aircraft rocket complexis SA-75M Dvina by the way, when was this spring in Israel the Day of air defence, so there hasn't been and this place was empty.
- in the picture 100_7182.jpg it is left to the missile 5V28 on OR 5P72 from anti-aircraft rocket complexis S-200VE Vega, the right is the rocket 5Ja23 to the OR SM-90 and belongs to the anti-aircraft rocket complexis S-75M* or higher
- in the picture Frame 104.jpg is rocket 1D to the OR SM-63 from the first version of the anti-aircraft rocket complexis SA-75 Dvina
Rocket 5Ja23 is not on the launch pad the SM-90, but SM-63 system SA-75 Dvina. It's basically a nonsensical combination of - volchovácká rocket on dviňáckém the launcher device. I didn't notice before, but Adminovy photos of it appeared in full nudity..
Not as it is but with the general denominations, which said Councils:
Quote :
basically goes on a nonsensical combination - volchovácká rocket on dviňáckém the launcher device.
In the implementation of PLRK S-75D Děsna (they were only in service with the army of the USSR), it was possible to use the rocket 11D, 13D, 13DA, 15D, 20D and 20DP, therefore, the rockets dviňácké i volchovské!.
Um, poor people couldn't get the ramp SM-90, the damage that I've personally drove six on the cancellation..

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Podle podkladů co mám by to ale měl být Volchov, ne Dvina.
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To bude vyžadovat hluboký ponor do archívu
