Major Shaitan Singh
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Promising heavy intercontinental ballistic missile. IDB Development is given no later than June 2009 ( according to an interview with the commander RSVN N.Solovtsova, 10.06.2009 ), and plans to create a missile by the end of 2016 ( source - the commander of the Strategic Missile Forces A.Shvaychenko, 16.12.2009 city ).
The purpose of the new heavy rocket - replacement in the Strategic Missile ICBM RS-20 / R-36 / the SS-18 SATAN . IDB Development is conducted SRC im.Makeeva (Miass, head developer) with the participation of NGO Engineering (Reutov, East -. Esin V., 2012, to Lenta.Ru ), as well as possible with the participation of "Southern" (Dnepropetrovsk, Ukraine, our hypothesis ).
Chief designer of the theme of "Sarmat" - M.G.Agafonov (2016, First Deputy General Designer SRC im.Makeeva, ist -. Designer №4 / 2016. ). As of October 2016 the chief designer of OCD "Sarmat" - Yu.A.Kaverin ( source .) Perhaps the earliest study ICBM variant were SRC im.Makeeva until 2005 ( source ). The state contract to perform OCD "Sarmat" signed between SRC im.Makeeva and the Ministry of defense of Russia in June, 2011 ( source ).
According to RIA "News" on May 8, 2012 the establishment of an ICBM being NPO Machine Building and will be completed no earlier than 2022
Design . According to sketchy reports in late 2010 - early 2011 gg It planned to consider draft (?) design of the complex and take reshanie the further development of an ICBM. Terms of reference for the development of IDB approved in 2011 ( ist -. Esin V., 2012, to Lenta.Ru ). The development of technical specifications for OCD "Sarmat" for prospective missile system with liquid ICBM was conducted with the participation of the Central Research Institute of the Ministry of Defense of Russia №4 ( source ).
In 2011, of the "Vanguard" has begun to develop technology and prescriptive feasibility of manufacturing the WPK rocket body ( source ) - this work is scheduled for completion in 2012. The development of materials for the preliminary design of onboard equipment for OCD "Sarmat" in terms of layout nodes meters of the angular velocity on the basis of a hemispherical resonator gyro prototyping and manufacturing six VTG samples of planned SPC automation and instrumentation for January-April 2012 ( source ).
According to the source 22 September 2012 "ended with a large (Science and Technology) on the Board of a new heavy rocket". All developers to 2-3 levels were represented at the council. October 19, 2012 IA "Interfax" reported that "in the beginning of October, the Ministry of Defence as a whole approved the preliminary design of the new heavy ICBM, but taking into account a number of comments and suggestions that developers should keep in mind during the further design, which has already begun ".
May 31, 2014 Deputy Minister of Defence Yury Borisov said that the work on the creation of heavy ICBMs go according to plan and that the new missile "can fly over the North and South Pole" ( source ). The name "SS-X-30" - conditional. Source 15A28 index - for example .
Image ICBM RS-28 "Sarmat" site SRC im.Makeeva, October 2016 ( source ).
The hypothetical image of an early version of the draft IDB Development im.Makeeva SRC,
which could form the basis of OCD "Sarmat", published in 2005 ( source ).
Development of rocket engines being NPO "Energomash" ( source ). On a competitive basis for the production of liquid propulsion 1st stage rocket Russian Ministry of Defence has selected the company PJSC "Proton-PM" ( "Perm Motors", Perm). In January 2013 it issued a technical specification for the development of promising propulsion system "product 99" and work began on the preparation of serial production. According to plans of 2013 to the end of 2014 is to be held the first firing test of the propulsion system. In 2014, the shipment is made to the customer four layouts "product 99" ( source 1 ). In 2014-2015 GG Work on the development of mass production continued, but, as of March 2016 stated that the development of production LRE "article 99" for the IDB behind schedule due to the novelty of the product ( source 2 ).
The tests . In a statement the media on 07/21/2015 was told that now runs the third stage of R & D to create complex and that the missiles will enter the flight test at the end of 2016-2017 GG The first ICBM for throwing test ready in November 2015 and of 16.12.2015 announced that before the end of 2015 the first test launch of the missile will take place at the cosmodrome Plesetsk. Later known as the date for throwing test in March 2016, however, 20 February 2016 reported that despite the willingness of the prototype test missiles are moved to the second quarter of 2016 due to the unavailability of the silos at the site Plesetsk. May 11, 2016 the media reported that test of an ICBM prototype throwing "Sarmat" postponed to the second half of 2016 due to unavailability of the rocket. Preparation launcher for testing at the site Plesetsk completed in April 2016, respectively, for about a year and can move all test charts and decision missiles on combat duty RVSN. Beginning of flight tests ICBM RS-28 "Sarmat" is expected in 2018 (Media , 09/07/2016, at the source .)
The production of ICBMs planned cooperation between enterprises formed SRC im.V.Makeeva - ie Krasnoyarsk Machine Building and dr.zavodami ( V.Esin, including 2012 ). The parent company for the production of advanced ICBMs samples "Sarmat" - Krasnoyarsk Machine-Building Plant. The contract with the plant to the production of prototypes allegedly concluded in 2011 with the delivery of the samples to the customer is likely in 2018 ( source ). June 18, 2013 RIA "News" reported that the construction of full-scale rocket sample starts in 2014 January 29, 2015 ( source ) reported plans to conduct in 2015 of throwing tests, apparently missiles layout followed beginning in 2016 -2017 GG missile flight tests. February 21, 2015 reported that at the Krasnoyarsk Machine-Building Plant has already manufactured the first elements of a new missile design.
In the first half of 2015 it was reported that razkety prototype for throwing tests will be performed in May and June 2015 of 06.26.2015 but it is reported that the completion of the prototype is scheduled for September and October - the deadline - the end of October 2015 . According to the source is made for about 60% of constructions vehicle (source ). Probably at the same plant will be carried out and mass production of the PC-28.
On the arming .According to the Chinese news "Xinhua" agency (from 05.05.2011), with reference to "Interfax" and the former Chief of Staff of the Strategic Missile Forces, Colonel-General Viktor Esin (as in 2012 - Advisor Commander of the Strategic Missile Force) planned production of a new ICBM combat duty since 2018 and the main developer of the MDBs is im.Makeeva SRC (Miass). September 3, 2012 in the media published a statement the commander of the Strategic Missile Forces, Colonel-General Sergei Karakaeva that the new heavy ICBM 100-ton class will be created by 2018 17.12.2013, commander of the Strategic Missile Forces, Colonel-General Sergei Karakayev again told the media that new missile system will go into the Strategic missile Forces in 2018-2020 GG ( Source ).
Placing missiles "Sarmat" is planned in Uzhur (Krasnoyarsk Territory) and Dombarovsky (Orenburg region) instead of missiles RS-20 / R-36 / the SS-18 SATAN (announced 25/12/2014 city). September 7, 2016 it was reported in the media. that the supply of ICBMs in the Strategic Missile Forces will begin no later than 2019 in Uzhur (Krasnoyarsk Territory) and Dombarovsky (Orenburg region) ( source ).
By 2007, the NGO Engineering and SRC them V.Makeeva completed joint research "Argument" which prompted the creation of ICBMs with a combination of technologies create domestic liquid ICBM and SLBM. Massa throws - 4350 kg Reach - 10,000 km results of research have shown that the creation of such rockets is possible within 7-8 years.
It was assumed as the use of the LRE rocket P-29RMU2 , motor step dilution warheads SLBM R-39UTTH . Reduced development costs assumed by the general unification of rocket units with other serial missiles. Estimated cost of development - 8.5 billion rubles.. RS-28 rocket launches Timeline "Sarmat":
Launcher - probably planned to use similar silo silos of R-36M / R-36M2 . For example, according to the source, the silos 15P718 complex on the site 106/109 polygon Cosmodrome as of 2009 it is planned technical upgrade, the customer - NGO Engineering ( ist -. 106 and 109 venues ... ).
Storage, transport and launch missiles from the assumed TPK development and production of the "Vanguard". In 2011 JSC "Avangard" has begun to develop technology and prescriptive feasibility of manufacturing the housing TPK "Sarmat" ( source ).
The control system and guidance - an inertial control system. At least nodes meters angular velocity on the basis of solid-state wave horoscope (VHG) developed by SPC Automation and Instrument them. Acad. N.A.Pilyugina. Development of materials for the preliminary design of onboard equipment for OCD "Sarmat" in the layout of the components of the angular velocity measuring devices based on a hemispherical resonator gyro and production of six prototypes VHG planned NCP Automation and Instrumentation in January-April 2012 ( source ).
As for soisipolnitelya OCD "Sarmat" was involved in 2011. manufacturer of measuring instruments "Institute" Hermes "(Zlatoust, source ). to ensure the telemetry on" Sarmat "department 121 SRC im.Makeeva developed an upgraded on-board telemetry system" Barracuda-M . "The system is the product of deep modernization of the telemetry system (STI)" Barracuda "has an extended composition in accordance with a number of new specific measurement tasks. As part MBRTS" Barracuda-M "there are 18 units for various purposes, including radio transmitting devices of its own design . to program and configure the devices of the system for a specific measurement program special program "Web" in section 121 is designed.
Among other unique features possessed by MBRTS "Barracuda-M", it is implemented the possibility of structural and algorithmic conversion of telemetry data (SAP TMI) to improve the noise immunity of data transmission. An important direction of the department is the development of the production base for the assembly layouts and product theme "Sarmat". Required to produce an annual "Barracuda-M" MBRTS hundreds of devices. To accomplish this task in the department with the assistance of 121 124 laboratory developed technological documentation for the production of the whole range of devices. Purchased equipment, which allowed to create a technological basis for the production of a new generation of competitive high-tech products.
Organized and certified six manufacturing sites: incoming inspection and packaging, mechanical, wiring, elektroproverok and prototyping, assembly and leak testing device housings, manufacture and application of adhesives and lacquers in microelectronic assembly ( . Ist - Fomin .)
Rocket design - multi-component longitudinal scheme (based on the first official image of ICBMs, October 2016): - PAD - stage 1 - stage 2 - stage 3 - the instrument compartment and breeding stage warheads - warhead Previously it was thought that the IDB includes in its composition and stage 2 block breeding warheads. LRE both stages "drowned" in the fuel tank, fuel tanks -. Bearing with combined separating bottoms Separation stages produced by piroshpangoutov ( source ). Block breeding warheads and layout warhead missiles allegedly made by the classical scheme for SRC im.Makeeva - martial blocks on the flight back. in 2013, of the "Vanguard" (g.Safronovo) within the framework of the ROC "Sarmat" will be launched mid OCD to develop material for the manufacture of elastic membrane shell adapter. The estimated cost of midrange OCD - 8.0 mln. Rub. ( Source ).
Engines : - Stage 1 (optional) - According to the annual report of "NPO Energomash named after academician VP Glushko" for 2012 15D285 NGOs engaged in the adaptation of the engine to be used in the first stage of an ICBM produced by OCD, "Sarmat". Since the propulsion 15D285 (RD-274) includes in its membership four LRE 15D286 (RD-273), ie predpolozheie that the new propulsion system based on two LRE 15D286 mass will be used missiles with a total thrust of the Earth 234.4 tons. There is also a likelihood that the propulsion system will be used in the second stage of the rocket. Description LRE 15D285 of articles on ICBM R-36M2 "Voivod" :
The structure of control 15D285 (RD-274) first stage unit 15S171 rocket consists of four independent single-chamber LRE 15D286 (RD-273), with turbopump fuel supply system carried out in a closed circuit with afterburning of oxidizer gas generator gas and pivotally mounted on the frame of the first stage of the tail compartment. Deviation engines Command Control System provides control of rocket flight.Engine Developer - KBEM (Chief Designer V.P.Radovsky). The proposal to upgrade the engines for the R-36M2, providing a boost traction and improved resistance to PFYAV, was received by the CB "Energomash" in 1980.Technical Proposal for the RD-263F engine development was published in December 1980. In March 1982, it released preliminary design for the development of modernized RD-274 (4 motor RD-273 unit) of the first stage.
Supposed to increase the gas pressure in the combustion chamber to 230 atm, to increase the rotational speed of the THA to 22500 / min. As a result, modifications of the engine thrust increased to 144 ton, specific impulse at the Earth's surface has increased to 296 kgf · s / kg. Finishing the test was completed in May 1985. Mass production engines were deployed at "Pivdenmash." - 1st stage (optional) - propulsion RC-99 ( source ) / "article 99" includes in its membership the RD-276 rocket engine (probably two). Serial production of LRE mastered PJSC "Proton-PM" ( "Perm Motors", Perm) in 2013-2016 (sources 3 and 4). As of March 2015 LRE design completed. It is the first product prototype assembly. Planned trials and in August 2015 the first shipment expected to set LRE missile manufacturer (source 5). June 9, 2015 at the shooting bench debug passed the first firing test of the prototype rocket engine "article 99" (source 6). Thrust RD-276 at the ground - 170 tons
RD-253 engine - the forerunner of RD-276 ( http://www.lpre.de/ ).
- 2nd stage - LRE development KBKhA - probably for the new ICBM will be upgraded previously developed LRE KBKhA ( source - Annual Report KBKhA in 2011 ).
- Step dilution warheads - probably LRE development KBHM im.Isaeva.
Start power unit . In the interest of creating a missile 15A28 (OCD "Sarmat") in 2015, work is underway on the development of power means starting 15D423 - probably hard fuel generators or engines ( source ). November 21, 2014 Krasnoyarsk Machine Building Plant has placed a request for production and delivery of prototypes 15D423 products and layouts in the amount of 550.8 million rubles. The application is available for delivery products only supplier - FTSDT "Union", Dzerzhinsk ( source ). In 2015, coating the detyalah "housing" 15D423 performs Perm Plant "Machine engineer", Perm ( source ).
TTX missiles : (geometric dimensions prikidochnye based on the estimated diameter of 3 m) Length: - with pad rocket - approx. 32 m - PAD - 2.15 m - 1 stage - GR.9 m - stage 2 - ok.8.9 m - 3 stage - ok.6 m Case diameter - 3 m Weight: - not less than 100,000 kg - 120-160 tons (forecast ,source )
Weight Throw-: - 4300 kg ( source ) - up to 5000 kg ( . ist - Esin V., to Lenta.Ru ) - up to 10,000 kg (Deputy Minister of defense Yu.Borisov, the data are not considered valid by us) - 5000- 5500 kg (forecast, source) Range - about 10000-11000 km CWE - 150-200 m (estimated)
warhead types : - no less than 8-10 MIRV with the perfect set of tools to overcome missile defense; - multiple maneuvering warheads (statement by the Deputy defense Minister Yury Borisov 31/05/2014, at the source .) - likely to be used as a carrier for 1-3-type object warheads 4202 / 15YU71 (our forecast of + power ).
Title : Russia - 2010 - The project is in the design, condition unknown . - 2012 on September 03 - in the media published a statement the commander of the Strategic missile Forces, Colonel-General Sergei Karakaeva that the new heavy ICBM 100-ton class will be created by 2018 - 2014 on December 25 - stated that the deployment of missile systems " Sarmat "is planned in Uzhur (Krasnoyarsk Territory) and Dombarovsky (Orenburg region) instead of missiles RS-20 / R-36 / the SS-18 SATAN .
Sources :Gundarov Q. missiles no false start. // Independent Military Review. 08.06.2007 city to Lenta.ru. 2009-2012 ggDefense Ministry approved the new IDB project. 2012 ( source ). MIC News. Website http://vpk.name , 2011Platform 106 and 109 of 2010 ( source ). Ptichkin S. Voivod in the fifth generation. // Russian newspaper. №5 / 2011 Sokolov "Execution can not be pardoned." Website http://www.arms-expo.ru , 2011 Fomin Ten years in telemetry. // Constructor. №4 / 2016 Dancomm. Website http://www.dancomm.ru/ , 2012 Russia to Adopt New Liquid Heavy ICBM after 2022. Site http://en.rian.ru , 2012
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The purpose of the new heavy rocket - replacement in the Strategic Missile ICBM RS-20 / R-36 / the SS-18 SATAN . IDB Development is conducted SRC im.Makeeva (Miass, head developer) with the participation of NGO Engineering (Reutov, East -. Esin V., 2012, to Lenta.Ru ), as well as possible with the participation of "Southern" (Dnepropetrovsk, Ukraine, our hypothesis ).
Chief designer of the theme of "Sarmat" - M.G.Agafonov (2016, First Deputy General Designer SRC im.Makeeva, ist -. Designer №4 / 2016. ). As of October 2016 the chief designer of OCD "Sarmat" - Yu.A.Kaverin ( source .) Perhaps the earliest study ICBM variant were SRC im.Makeeva until 2005 ( source ). The state contract to perform OCD "Sarmat" signed between SRC im.Makeeva and the Ministry of defense of Russia in June, 2011 ( source ).
According to RIA "News" on May 8, 2012 the establishment of an ICBM being NPO Machine Building and will be completed no earlier than 2022
Design . According to sketchy reports in late 2010 - early 2011 gg It planned to consider draft (?) design of the complex and take reshanie the further development of an ICBM. Terms of reference for the development of IDB approved in 2011 ( ist -. Esin V., 2012, to Lenta.Ru ). The development of technical specifications for OCD "Sarmat" for prospective missile system with liquid ICBM was conducted with the participation of the Central Research Institute of the Ministry of Defense of Russia №4 ( source ).
In 2011, of the "Vanguard" has begun to develop technology and prescriptive feasibility of manufacturing the WPK rocket body ( source ) - this work is scheduled for completion in 2012. The development of materials for the preliminary design of onboard equipment for OCD "Sarmat" in terms of layout nodes meters of the angular velocity on the basis of a hemispherical resonator gyro prototyping and manufacturing six VTG samples of planned SPC automation and instrumentation for January-April 2012 ( source ).
According to the source 22 September 2012 "ended with a large (Science and Technology) on the Board of a new heavy rocket". All developers to 2-3 levels were represented at the council. October 19, 2012 IA "Interfax" reported that "in the beginning of October, the Ministry of Defence as a whole approved the preliminary design of the new heavy ICBM, but taking into account a number of comments and suggestions that developers should keep in mind during the further design, which has already begun ".
May 31, 2014 Deputy Minister of Defence Yury Borisov said that the work on the creation of heavy ICBMs go according to plan and that the new missile "can fly over the North and South Pole" ( source ). The name "SS-X-30" - conditional. Source 15A28 index - for example .
Image ICBM RS-28 "Sarmat" site SRC im.Makeeva, October 2016 ( source ).
The hypothetical image of an early version of the draft IDB Development im.Makeeva SRC,
which could form the basis of OCD "Sarmat", published in 2005 ( source ).
Development of rocket engines being NPO "Energomash" ( source ). On a competitive basis for the production of liquid propulsion 1st stage rocket Russian Ministry of Defence has selected the company PJSC "Proton-PM" ( "Perm Motors", Perm). In January 2013 it issued a technical specification for the development of promising propulsion system "product 99" and work began on the preparation of serial production. According to plans of 2013 to the end of 2014 is to be held the first firing test of the propulsion system. In 2014, the shipment is made to the customer four layouts "product 99" ( source 1 ). In 2014-2015 GG Work on the development of mass production continued, but, as of March 2016 stated that the development of production LRE "article 99" for the IDB behind schedule due to the novelty of the product ( source 2 ).
The tests . In a statement the media on 07/21/2015 was told that now runs the third stage of R & D to create complex and that the missiles will enter the flight test at the end of 2016-2017 GG The first ICBM for throwing test ready in November 2015 and of 16.12.2015 announced that before the end of 2015 the first test launch of the missile will take place at the cosmodrome Plesetsk. Later known as the date for throwing test in March 2016, however, 20 February 2016 reported that despite the willingness of the prototype test missiles are moved to the second quarter of 2016 due to the unavailability of the silos at the site Plesetsk. May 11, 2016 the media reported that test of an ICBM prototype throwing "Sarmat" postponed to the second half of 2016 due to unavailability of the rocket. Preparation launcher for testing at the site Plesetsk completed in April 2016, respectively, for about a year and can move all test charts and decision missiles on combat duty RVSN. Beginning of flight tests ICBM RS-28 "Sarmat" is expected in 2018 (Media , 09/07/2016, at the source .)
The production of ICBMs planned cooperation between enterprises formed SRC im.V.Makeeva - ie Krasnoyarsk Machine Building and dr.zavodami ( V.Esin, including 2012 ). The parent company for the production of advanced ICBMs samples "Sarmat" - Krasnoyarsk Machine-Building Plant. The contract with the plant to the production of prototypes allegedly concluded in 2011 with the delivery of the samples to the customer is likely in 2018 ( source ). June 18, 2013 RIA "News" reported that the construction of full-scale rocket sample starts in 2014 January 29, 2015 ( source ) reported plans to conduct in 2015 of throwing tests, apparently missiles layout followed beginning in 2016 -2017 GG missile flight tests. February 21, 2015 reported that at the Krasnoyarsk Machine-Building Plant has already manufactured the first elements of a new missile design.
In the first half of 2015 it was reported that razkety prototype for throwing tests will be performed in May and June 2015 of 06.26.2015 but it is reported that the completion of the prototype is scheduled for September and October - the deadline - the end of October 2015 . According to the source is made for about 60% of constructions vehicle (source ). Probably at the same plant will be carried out and mass production of the PC-28.
On the arming .According to the Chinese news "Xinhua" agency (from 05.05.2011), with reference to "Interfax" and the former Chief of Staff of the Strategic Missile Forces, Colonel-General Viktor Esin (as in 2012 - Advisor Commander of the Strategic Missile Force) planned production of a new ICBM combat duty since 2018 and the main developer of the MDBs is im.Makeeva SRC (Miass). September 3, 2012 in the media published a statement the commander of the Strategic Missile Forces, Colonel-General Sergei Karakaeva that the new heavy ICBM 100-ton class will be created by 2018 17.12.2013, commander of the Strategic Missile Forces, Colonel-General Sergei Karakayev again told the media that new missile system will go into the Strategic missile Forces in 2018-2020 GG ( Source ).
Placing missiles "Sarmat" is planned in Uzhur (Krasnoyarsk Territory) and Dombarovsky (Orenburg region) instead of missiles RS-20 / R-36 / the SS-18 SATAN (announced 25/12/2014 city). September 7, 2016 it was reported in the media. that the supply of ICBMs in the Strategic Missile Forces will begin no later than 2019 in Uzhur (Krasnoyarsk Territory) and Dombarovsky (Orenburg region) ( source ).
By 2007, the NGO Engineering and SRC them V.Makeeva completed joint research "Argument" which prompted the creation of ICBMs with a combination of technologies create domestic liquid ICBM and SLBM. Massa throws - 4350 kg Reach - 10,000 km results of research have shown that the creation of such rockets is possible within 7-8 years.
It was assumed as the use of the LRE rocket P-29RMU2 , motor step dilution warheads SLBM R-39UTTH . Reduced development costs assumed by the general unification of rocket units with other serial missiles. Estimated cost of development - 8.5 billion rubles.. RS-28 rocket launches Timeline "Sarmat":
Launcher - probably planned to use similar silo silos of R-36M / R-36M2 . For example, according to the source, the silos 15P718 complex on the site 106/109 polygon Cosmodrome as of 2009 it is planned technical upgrade, the customer - NGO Engineering ( ist -. 106 and 109 venues ... ).
Storage, transport and launch missiles from the assumed TPK development and production of the "Vanguard". In 2011 JSC "Avangard" has begun to develop technology and prescriptive feasibility of manufacturing the housing TPK "Sarmat" ( source ).
The control system and guidance - an inertial control system. At least nodes meters angular velocity on the basis of solid-state wave horoscope (VHG) developed by SPC Automation and Instrument them. Acad. N.A.Pilyugina. Development of materials for the preliminary design of onboard equipment for OCD "Sarmat" in the layout of the components of the angular velocity measuring devices based on a hemispherical resonator gyro and production of six prototypes VHG planned NCP Automation and Instrumentation in January-April 2012 ( source ).
As for soisipolnitelya OCD "Sarmat" was involved in 2011. manufacturer of measuring instruments "Institute" Hermes "(Zlatoust, source ). to ensure the telemetry on" Sarmat "department 121 SRC im.Makeeva developed an upgraded on-board telemetry system" Barracuda-M . "The system is the product of deep modernization of the telemetry system (STI)" Barracuda "has an extended composition in accordance with a number of new specific measurement tasks. As part MBRTS" Barracuda-M "there are 18 units for various purposes, including radio transmitting devices of its own design . to program and configure the devices of the system for a specific measurement program special program "Web" in section 121 is designed.
Among other unique features possessed by MBRTS "Barracuda-M", it is implemented the possibility of structural and algorithmic conversion of telemetry data (SAP TMI) to improve the noise immunity of data transmission. An important direction of the department is the development of the production base for the assembly layouts and product theme "Sarmat". Required to produce an annual "Barracuda-M" MBRTS hundreds of devices. To accomplish this task in the department with the assistance of 121 124 laboratory developed technological documentation for the production of the whole range of devices. Purchased equipment, which allowed to create a technological basis for the production of a new generation of competitive high-tech products.
Organized and certified six manufacturing sites: incoming inspection and packaging, mechanical, wiring, elektroproverok and prototyping, assembly and leak testing device housings, manufacture and application of adhesives and lacquers in microelectronic assembly ( . Ist - Fomin .)
Rocket design - multi-component longitudinal scheme (based on the first official image of ICBMs, October 2016): - PAD - stage 1 - stage 2 - stage 3 - the instrument compartment and breeding stage warheads - warhead Previously it was thought that the IDB includes in its composition and stage 2 block breeding warheads. LRE both stages "drowned" in the fuel tank, fuel tanks -. Bearing with combined separating bottoms Separation stages produced by piroshpangoutov ( source ). Block breeding warheads and layout warhead missiles allegedly made by the classical scheme for SRC im.Makeeva - martial blocks on the flight back. in 2013, of the "Vanguard" (g.Safronovo) within the framework of the ROC "Sarmat" will be launched mid OCD to develop material for the manufacture of elastic membrane shell adapter. The estimated cost of midrange OCD - 8.0 mln. Rub. ( Source ).
Engines : - Stage 1 (optional) - According to the annual report of "NPO Energomash named after academician VP Glushko" for 2012 15D285 NGOs engaged in the adaptation of the engine to be used in the first stage of an ICBM produced by OCD, "Sarmat". Since the propulsion 15D285 (RD-274) includes in its membership four LRE 15D286 (RD-273), ie predpolozheie that the new propulsion system based on two LRE 15D286 mass will be used missiles with a total thrust of the Earth 234.4 tons. There is also a likelihood that the propulsion system will be used in the second stage of the rocket. Description LRE 15D285 of articles on ICBM R-36M2 "Voivod" :
The structure of control 15D285 (RD-274) first stage unit 15S171 rocket consists of four independent single-chamber LRE 15D286 (RD-273), with turbopump fuel supply system carried out in a closed circuit with afterburning of oxidizer gas generator gas and pivotally mounted on the frame of the first stage of the tail compartment. Deviation engines Command Control System provides control of rocket flight.Engine Developer - KBEM (Chief Designer V.P.Radovsky). The proposal to upgrade the engines for the R-36M2, providing a boost traction and improved resistance to PFYAV, was received by the CB "Energomash" in 1980.Technical Proposal for the RD-263F engine development was published in December 1980. In March 1982, it released preliminary design for the development of modernized RD-274 (4 motor RD-273 unit) of the first stage.
Supposed to increase the gas pressure in the combustion chamber to 230 atm, to increase the rotational speed of the THA to 22500 / min. As a result, modifications of the engine thrust increased to 144 ton, specific impulse at the Earth's surface has increased to 296 kgf · s / kg. Finishing the test was completed in May 1985. Mass production engines were deployed at "Pivdenmash." - 1st stage (optional) - propulsion RC-99 ( source ) / "article 99" includes in its membership the RD-276 rocket engine (probably two). Serial production of LRE mastered PJSC "Proton-PM" ( "Perm Motors", Perm) in 2013-2016 (sources 3 and 4). As of March 2015 LRE design completed. It is the first product prototype assembly. Planned trials and in August 2015 the first shipment expected to set LRE missile manufacturer (source 5). June 9, 2015 at the shooting bench debug passed the first firing test of the prototype rocket engine "article 99" (source 6). Thrust RD-276 at the ground - 170 tons
RD-253 engine - the forerunner of RD-276 ( http://www.lpre.de/ ).
- 2nd stage - LRE development KBKhA - probably for the new ICBM will be upgraded previously developed LRE KBKhA ( source - Annual Report KBKhA in 2011 ).
- Step dilution warheads - probably LRE development KBHM im.Isaeva.
Start power unit . In the interest of creating a missile 15A28 (OCD "Sarmat") in 2015, work is underway on the development of power means starting 15D423 - probably hard fuel generators or engines ( source ). November 21, 2014 Krasnoyarsk Machine Building Plant has placed a request for production and delivery of prototypes 15D423 products and layouts in the amount of 550.8 million rubles. The application is available for delivery products only supplier - FTSDT "Union", Dzerzhinsk ( source ). In 2015, coating the detyalah "housing" 15D423 performs Perm Plant "Machine engineer", Perm ( source ).
TTX missiles : (geometric dimensions prikidochnye based on the estimated diameter of 3 m) Length: - with pad rocket - approx. 32 m - PAD - 2.15 m - 1 stage - GR.9 m - stage 2 - ok.8.9 m - 3 stage - ok.6 m Case diameter - 3 m Weight: - not less than 100,000 kg - 120-160 tons (forecast ,source )
Weight Throw-: - 4300 kg ( source ) - up to 5000 kg ( . ist - Esin V., to Lenta.Ru ) - up to 10,000 kg (Deputy Minister of defense Yu.Borisov, the data are not considered valid by us) - 5000- 5500 kg (forecast, source) Range - about 10000-11000 km CWE - 150-200 m (estimated)
warhead types : - no less than 8-10 MIRV with the perfect set of tools to overcome missile defense; - multiple maneuvering warheads (statement by the Deputy defense Minister Yury Borisov 31/05/2014, at the source .) - likely to be used as a carrier for 1-3-type object warheads 4202 / 15YU71 (our forecast of + power ).
Title : Russia - 2010 - The project is in the design, condition unknown . - 2012 on September 03 - in the media published a statement the commander of the Strategic missile Forces, Colonel-General Sergei Karakaeva that the new heavy ICBM 100-ton class will be created by 2018 - 2014 on December 25 - stated that the deployment of missile systems " Sarmat "is planned in Uzhur (Krasnoyarsk Territory) and Dombarovsky (Orenburg region) instead of missiles RS-20 / R-36 / the SS-18 SATAN .
Sources :Gundarov Q. missiles no false start. // Independent Military Review. 08.06.2007 city to Lenta.ru. 2009-2012 ggDefense Ministry approved the new IDB project. 2012 ( source ). MIC News. Website http://vpk.name , 2011Platform 106 and 109 of 2010 ( source ). Ptichkin S. Voivod in the fifth generation. // Russian newspaper. №5 / 2011 Sokolov "Execution can not be pardoned." Website http://www.arms-expo.ru , 2011 Fomin Ten years in telemetry. // Constructor. №4 / 2016 Dancomm. Website http://www.dancomm.ru/ , 2012 Russia to Adopt New Liquid Heavy ICBM after 2022. Site http://en.rian.ru , 2012
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