超级军网伊斯坎德尔的前辈--SS-23蜘蛛短程弹道导弹简析
来源：百度文库 编辑：超级军网 时间：2024/05/02 00:29:49
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背景交代：
Complex 9K714 Oka, missile 9M714 / OTR-23 - SS-23 SPIDER-A
rocket 9M714U - SS-23 SPIDER-B / KY-19
P-400 - export item
Intelligence and Army tactical missile system managers. The development was carried out in KBM (Kolomna, then - MSC) under the leadership of SP Invincible apparently from 1972 with leverage from the project "Rota" and "Uranus". Testing of the missile began in 1976, the state tests were conducted at Kapustin Yar in 1977-1979 (produced according to various sources 26 or 31 start). Serial production of missiles were built at the Votkinsk machine works since 1976, the Socialist Party and machines to ensure - in Petropavlovsk Plant of Heavy Machinery (from 1979 to 1987).
Complex 9K714 Oka adopted in the 1980 (in 1983 to dr.dannym) and began to enter the army partly replacing complexes 9K72 Scud-B. The structure of the USSR Armed Forces set to be used as a high-precision combat element of surveillance and strike (DCR), and reconnaissance of fire (ROC) complexes. In 1981, the complex was detected by Western intelligence means, and identified as SS-23 SPIDER. In December 1987 a set of restrictions came under the Treaty on the Reduction of INF and was reduced. Work on the modification of the Oka-U were terminated in 1987 in preparation for mass production and the adoption of. The name "OTR-23" was used in the documentation for the INF Treaty with the reduction. By default, the data base missile 9M714.
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Tentative projection variants 9M714 missile complex 9K714 Oka "/ SS-23 SPIDER (c)
20.12.2009
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--
Test launch tactical 9M714 complex 9K714 Oka
(shots from the film "Impact force / Rocket Wide Web, television, Ostankino, 2008)
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--
9M714 missile at the Museum of the USSR Armed Forces and Russia
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背景交代：
Complex 9K714 Oka, missile 9M714 / OTR-23 - SS-23 SPIDER-A
rocket 9M714U - SS-23 SPIDER-B / KY-19
P-400 - export item
Intelligence and Army tactical missile system managers. The development was carried out in KBM (Kolomna, then - MSC) under the leadership of SP Invincible apparently from 1972 with leverage from the project "Rota" and "Uranus". Testing of the missile began in 1976, the state tests were conducted at Kapustin Yar in 1977-1979 (produced according to various sources 26 or 31 start). Serial production of missiles were built at the Votkinsk machine works since 1976, the Socialist Party and machines to ensure - in Petropavlovsk Plant of Heavy Machinery (from 1979 to 1987).
Complex 9K714 Oka adopted in the 1980 (in 1983 to dr.dannym) and began to enter the army partly replacing complexes 9K72 Scud-B. The structure of the USSR Armed Forces set to be used as a high-precision combat element of surveillance and strike (DCR), and reconnaissance of fire (ROC) complexes. In 1981, the complex was detected by Western intelligence means, and identified as SS-23 SPIDER. In December 1987 a set of restrictions came under the Treaty on the Reduction of INF and was reduced. Work on the modification of the Oka-U were terminated in 1987 in preparation for mass production and the adoption of. The name "OTR-23" was used in the documentation for the INF Treaty with the reduction. By default, the data base missile 9M714.
========
Tentative projection variants 9M714 missile complex 9K714 Oka "/ SS-23 SPIDER (c)
20.12.2009
--
--
Test launch tactical 9M714 complex 9K714 Oka
(shots from the film "Impact force / Rocket Wide Web, television, Ostankino, 2008)
--
--
9M714 missile at the Museum of the USSR Armed Forces and Russia
--
==============================
导弹的控制系统：
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Crossing - the missile's control system is an autonomous inertial (development GosNIIAG), correction of the trajectory carried on the active site with the help of rotary engine nozzles and throughout the flight with the help of lattice aerodynamic control surfaces. The structure of control equipment includes gyrostabilized 9B86 platform with sensors of angular velocities and accelerations, as well as sensors NIEs (zero-rate indicator - for determining the lateral velocity).
Department Warhead occurred outside the atmosphere on a downward trajectory. The trajectory of the final phase of flight Warhead - almost vertical drop. To equip tactical warheads "Oka" in GosTsNIRTI (VI Kupriyanov chief designer) was a complex means to overcome missile defense. Sector targeting missiles at start 180 deg. System aiming at SPU - optoelectronic 9SH133 (similar to the system aiming tactical "Point").
Aiming missiles carried in the horizontal position of the STC. Towards the goal of unfolding gyrostabilized platform in command and gyroscopic devices. After launch the missile turns toward the goal, practicing entered the corner. Due to a change in angle of rotation of the rocket after launch may be redirected quickly without overcharging rocket launcher in the sector of 180 degrees. Office missile in flight by turning the engine nozzles and lattice aerodynamic control surfaces. At the end of the active region of the trajectory control system continues to work. Upon entering the atmosphere trellised aerodynamic control surfaces guided missile on a downward trajectory, thereby increasing accuracy.
To counter the defense used by almost all available fundsat the time:
- Maneuver after launch.
- Unusually high trajectory
- High speed
- Insulation liner warhead
- Dispersed after the separation of warheads active and passive noise and simulators Warhead
For difficulties precision missile in the active phase of the trajectory in order to make the flames flicker in the fuel could be introduced special additives (theoretically is possible, but on the practical implementation of the no).
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Gyrocompass sighting system 9SH133
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----
Command and gyroscopic devices. Well visible gyrostabilized platform 9B86
--
---------
There are at least three modifications of GFP in different buildings
The Oka-U - radar homing warheads and on the aerodynamic control surfaces on the warheads for guidance on the final trajectory. It is possible to use in the surveillance and strike systems to obtain targeting information from a remote source with the adjustment and re-direct warheads in the middle of the trajectory (from aircraft reconnaissance and AWACS).
==============================
导弹的控制系统：
--
Crossing - the missile's control system is an autonomous inertial (development GosNIIAG), correction of the trajectory carried on the active site with the help of rotary engine nozzles and throughout the flight with the help of lattice aerodynamic control surfaces. The structure of control equipment includes gyrostabilized 9B86 platform with sensors of angular velocities and accelerations, as well as sensors NIEs (zero-rate indicator - for determining the lateral velocity).
Department Warhead occurred outside the atmosphere on a downward trajectory. The trajectory of the final phase of flight Warhead - almost vertical drop. To equip tactical warheads "Oka" in GosTsNIRTI (VI Kupriyanov chief designer) was a complex means to overcome missile defense. Sector targeting missiles at start 180 deg. System aiming at SPU - optoelectronic 9SH133 (similar to the system aiming tactical "Point").
Aiming missiles carried in the horizontal position of the STC. Towards the goal of unfolding gyrostabilized platform in command and gyroscopic devices. After launch the missile turns toward the goal, practicing entered the corner. Due to a change in angle of rotation of the rocket after launch may be redirected quickly without overcharging rocket launcher in the sector of 180 degrees. Office missile in flight by turning the engine nozzles and lattice aerodynamic control surfaces. At the end of the active region of the trajectory control system continues to work. Upon entering the atmosphere trellised aerodynamic control surfaces guided missile on a downward trajectory, thereby increasing accuracy.
To counter the defense used by almost all available fundsat the time:
- Maneuver after launch.
- Unusually high trajectory
- High speed
- Insulation liner warhead
- Dispersed after the separation of warheads active and passive noise and simulators Warhead
For difficulties precision missile in the active phase of the trajectory in order to make the flames flicker in the fuel could be introduced special additives (theoretically is possible, but on the practical implementation of the no).
------
Gyrocompass sighting system 9SH133
--
----
Command and gyroscopic devices. Well visible gyrostabilized platform 9B86
--
---------
There are at least three modifications of GFP in different buildings
The Oka-U - radar homing warheads and on the aerodynamic control surfaces on the warheads for guidance on the final trajectory. It is possible to use in the surveillance and strike systems to obtain targeting information from a remote source with the adjustment and re-direct warheads in the middle of the trajectory (from aircraft reconnaissance and AWACS).
=========================
发射载车系统：
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Launcher:
Complex 9K714 Oka - wheel amphibious STC 9P71 chassis BAZ-6944 "Basis-1" (one missile at the STC and two on TZM). TZM 9T230 performed on the same chassis and equipped with a crane. Installations designed SKB-221 (CDB "Titan") and prototypes are produced at the plant "Barricades". Mass production was carried Petropavlovsk Heavy Machine Building Plant (1979-1987 yy). Propulsion on the water - 2 waterjet.
STC and TZM were aviatrasportabelny IL-76, AN-22. At the STC installed topographic location and aiming missiles 1T125 with panel 9V553 guidance system, the system checks and launch rockets 9V170. Aiming the missile is in its horizontal position on the inside SPU with opto-electronic system 9SH133 (similar to the system aiming OTP "Point"). At TZM installed navigation system TNA-4.
TTX STC and TZM:
Engine - diesel engine UTD-25 / D-144 400 hp and generator VG-7500N
Wheel arrangement - 8 x 8 (the first two-axis turning)
Length - 11760 mm (STC), 11800 mm (TLV)
Width - 3128 mm (STC), 3128 mm (TLV)
Height (field position) - 3000 mm (STC and TZM)
The height of the rocket in the starting position - 10130 mm
The angle of elevation of the rocket launch - 82 deg
Weight - 24070 kg (without missiles), 29100 kg (STCs with a missile), 29985 kg (TZM, 28685 kg dr.dannym)
Calculation - 3 people. (STC, TLV)
Speed on the highway - 65 km / h (70 km / h on dr.dannym)
Speed along the ground - 20-40 km / h
Speed afloat - 8-10 km / h
Cruising range - 700 miles (1000 km on dr.dannym)
Crane capacity to TZM - 5000 kg
==========================
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STC 9P71 complex 9K714 Oka on tests (a frame from the movie "Impact force / Rocket Wide Web, television, Ostankino, 2008)
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TZM 9T230 on tests
--
[
--
TZM 9T230 on trials afloat
--
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Shows air transportability STC 9P71 "Oka" IL-76
--
--
STC 9P71 with a missile 9M714 with ionizing (or nuclear, inert) warhead in the process of recovery in the preparation of the launch
--
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STC 9P71, apparently all the images show "Oka" army
Slovakia - the top for sure - with the usual missile warheads
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"Filling" STC complex 9K714 Oka Museum in Sofia, Bulgaria. It is clearly seen Thermal protective shield for the missile warheads
--
--
The commander of calculation 9P71: from left to right - the remote control system of survey 1T125, panel tablet system of survey (in which the embedded map area) 9V553 and control panel testing and launching rockets 9V17
--
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Remote system of survey and guidance 1T125 with tablet toporivyazki
--
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STC or TZM "Oka-U chassis BAZ-69481
--
=========================
发射载车系统：
--
Launcher:
Complex 9K714 Oka - wheel amphibious STC 9P71 chassis BAZ-6944 "Basis-1" (one missile at the STC and two on TZM). TZM 9T230 performed on the same chassis and equipped with a crane. Installations designed SKB-221 (CDB "Titan") and prototypes are produced at the plant "Barricades". Mass production was carried Petropavlovsk Heavy Machine Building Plant (1979-1987 yy). Propulsion on the water - 2 waterjet.
STC and TZM were aviatrasportabelny IL-76, AN-22. At the STC installed topographic location and aiming missiles 1T125 with panel 9V553 guidance system, the system checks and launch rockets 9V170. Aiming the missile is in its horizontal position on the inside SPU with opto-electronic system 9SH133 (similar to the system aiming OTP "Point"). At TZM installed navigation system TNA-4.
TTX STC and TZM:
Engine - diesel engine UTD-25 / D-144 400 hp and generator VG-7500N
Wheel arrangement - 8 x 8 (the first two-axis turning)
Length - 11760 mm (STC), 11800 mm (TLV)
Width - 3128 mm (STC), 3128 mm (TLV)
Height (field position) - 3000 mm (STC and TZM)
The height of the rocket in the starting position - 10130 mm
The angle of elevation of the rocket launch - 82 deg
Weight - 24070 kg (without missiles), 29100 kg (STCs with a missile), 29985 kg (TZM, 28685 kg dr.dannym)
Calculation - 3 people. (STC, TLV)
Speed on the highway - 65 km / h (70 km / h on dr.dannym)
Speed along the ground - 20-40 km / h
Speed afloat - 8-10 km / h
Cruising range - 700 miles (1000 km on dr.dannym)
Crane capacity to TZM - 5000 kg
==========================
--
STC 9P71 complex 9K714 Oka on tests (a frame from the movie "Impact force / Rocket Wide Web, television, Ostankino, 2008)
--
-------
TZM 9T230 on tests
--
[
--
TZM 9T230 on trials afloat
--
------
Shows air transportability STC 9P71 "Oka" IL-76
--
--
STC 9P71 with a missile 9M714 with ionizing (or nuclear, inert) warhead in the process of recovery in the preparation of the launch
--
----------
STC 9P71, apparently all the images show "Oka" army
Slovakia - the top for sure - with the usual missile warheads
--
-------
"Filling" STC complex 9K714 Oka Museum in Sofia, Bulgaria. It is clearly seen Thermal protective shield for the missile warheads
--
--
The commander of calculation 9P71: from left to right - the remote control system of survey 1T125, panel tablet system of survey (in which the embedded map area) 9V553 and control panel testing and launching rockets 9V17
--
--------
Remote system of survey and guidance 1T125 with tablet toporivyazki
--
-------
STC or TZM "Oka-U chassis BAZ-69481
--
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未完待续.......................
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未完待续.......................
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期待中。。。。。。
坐等翻译帝{:yan:}
这车不错，水陆两用……
就是这车，还有种6乘6的，不知是什么型号，俄文也看不懂
Please change into chinese
俺庄户人不懂外语
俺庄户人不懂外语
帖子太监了？刺激刺激！
这个和楼主所贴的车型挺类似，只不过是6乘6的，也是MAZ的作品。
这个和楼主所贴的车型挺类似，只不过是6乘6的，也是MAZ的作品。
回复 10# luyuanrui
你的图注上很明显是BAZ-5921，那就应该是布良斯克汽车厂的作品
你的图注上很明显是BAZ-5921，那就应该是布良斯克汽车厂的作品
“蜘蛛”也毁于戈尔巴乔夫的妥协政策，西方利用他这种弱点将此也加入削减名单并得到其最终批准，苏联的首款比较精确的短程弹道导弹...{:yan:}
luzhen_sh323 发表于 2009-12-24 00:48 
现在BAZ 当道了。 在S-400， Pantirs防空系统， 都是BAZ系列了。
MAZ除非被整合， 否则慢慢的淡出。
现在BAZ 当道了。 在S-400， Pantirs防空系统， 都是BAZ系列了。
MAZ除非被整合， 否则慢慢的淡出。
LZ怎么了？
LZ已经人间蒸发
短程看好SS－21
短程看好SS－21
回复 11# luzhen_sh323
哦，多谢，其实我看不懂俄文
哦，多谢，其实我看不懂俄文
回复 16# luyuanrui
呵呵，其实我也看不懂毛文:handshake不过学了一个笨办法，看着那字母像B就说是B了~~~:lol
呵呵，其实我也看不懂毛文:handshake不过学了一个笨办法，看着那字母像B就说是B了~~~:lol
六千 发表于 2009-12-24 02:49
估计又骂人被关小黑屋了~~~:D
估计又骂人被关小黑屋了~~~:D
进来时发觉兰州已经杯具了
估计是在空版杯具的……
估计是在空版杯具的……
兰州不是已经进去过一次了吗？这次二进宫啊！是终身监禁不得假释那种不？还能出来吧？
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格珊设计在R-77中..............
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格珊设计在R-77中..............
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Missile 9M714 - the number of steps - 1 (Rocket block of reinforced carbon fiber with a thermal layer). The design consists of a rocket engine compartment with a nozzle unit with aerodynamic control surfaces (the gabartno-weight models of missiles trellised aerodynamic control surfaces are made in the shape of a frame with two diagonal ridges), the instrument compartment, the transfer compartment and detachable warhead. Transfer module with the nuclear warheads and conventional warheads differed. Usually in the transitional compartment housed false targets and sources of interference (see below - Battle of). Department Warhead is shooting explosive bolts and the braking rocket engine block. Storage and transportation of the missile unit was carried out (if necessary) in a container 9YA249, the transfer module - a container 9YA258.
Engines - 1 x solid propellant rocket motors, 4 rotary nozzle with two degrees of freedom associated with aerodynamic control surfaces. At the stage of research and assumed the additional engine promotion, which should give the rotation a breakaway Warhead in order to improve accuracy, but in the process of testing to improve the accuracy of Warhead has not happened in the series of special warheads engine promotion is not connected to a control system (see below - Battle of) . At the bottom of the SRBs in the case of missile unit on a circle are the windows zero draft, which the team of APR (emergency undermine missiles) reveals the lifting charge, the pressure in the combustion chamber is reduced and the engine stops working. To control nozzles and aerodynamic control surfaces are designed servos 9B89 for work which involved gasifier 9D153. Power of all systems of the missile is provided turbogenerator 9D154.
Thrust front - 14820 kg
Hours RDTT maximum - 70
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Engine missile 9M714 . The numbers denote: 1 - Mechanical part of the case solid propellant rocket motors, 2 - a charge of fuel, 3 - cylindrical shell, 4 - valve, 5 - hoop-buckle, 6 - posterior part of the solid propellant rocket motors; 7 - rotating nozzle, 8 - Mechanical part of the body SRBs, 9 - the main bulwark of solid propellant rocket motors, 10 - primer, 11 - cover, 12 and 13 - Thermal protection;
--
---------
Nozzle engine block OTR 9M714 "Oka at the exhibition IDET-1994
In front of the missile unit installed engine brake used for braking rocket unit in the department of warheads
--
--------
Brake rocket engine 9M714
--
--
Length:
- 7520 mm (9M714, 9M714K - on questionable data)
- 7315 mm (9M714K)
- 7516 mm (9M714B, 9M714UT)
The length of the block without a missile warheads - 5170 mm
Diameter - 974 mm
A swing-open lattice rudders - 1848 mm
Weight:
- 4400-4690 kg
- 4630 kg (9M714K)
- 4400 kg (9M714B)
- 4480 kg (9M714B1)
Weight without warheads - 3990 kg
Warhead weight - 372-715 kg
Weight-cone adapter to connect the unit with rocket warheads - 80 kg
Range:
- 50 km (minimum, 9M714)
- 300 km (9M714K)
- 400 km (9M714B, according TTX)
- 407-450 km (maximum 9M714, depending on the type of warhead, but 9M714K)
- 500 km (Oka-U, up to 700 km stage design)
The height of the top point of the trajectory - 120 km
The rocket's velocity at the end of the active region of the trajectory - 4 M
Speed warheads in the final stage - 10 M
CEP:
- 50-150 m (Oka, 350 m from dr.dannym)
- 30 m (Oka-U)
Hours charge elektroturbogeneratora missiles - with 97,5
Deployment time from march - 5 minutes (?)
Time ready for launch in March - 3 min
Lifting time rocket from the transport situation in the starter - 20 p.
Time replacement warheads on the STC - 15 minutes
Time guaranteed storage - 10 years
Time to guarantee the storage in the field - 3 years
Missile 9M714 - the number of steps - 1 (Rocket block of reinforced carbon fiber with a thermal layer). The design consists of a rocket engine compartment with a nozzle unit with aerodynamic control surfaces (the gabartno-weight models of missiles trellised aerodynamic control surfaces are made in the shape of a frame with two diagonal ridges), the instrument compartment, the transfer compartment and detachable warhead. Transfer module with the nuclear warheads and conventional warheads differed. Usually in the transitional compartment housed false targets and sources of interference (see below - Battle of). Department Warhead is shooting explosive bolts and the braking rocket engine block. Storage and transportation of the missile unit was carried out (if necessary) in a container 9YA249, the transfer module - a container 9YA258.
Engines - 1 x solid propellant rocket motors, 4 rotary nozzle with two degrees of freedom associated with aerodynamic control surfaces. At the stage of research and assumed the additional engine promotion, which should give the rotation a breakaway Warhead in order to improve accuracy, but in the process of testing to improve the accuracy of Warhead has not happened in the series of special warheads engine promotion is not connected to a control system (see below - Battle of) . At the bottom of the SRBs in the case of missile unit on a circle are the windows zero draft, which the team of APR (emergency undermine missiles) reveals the lifting charge, the pressure in the combustion chamber is reduced and the engine stops working. To control nozzles and aerodynamic control surfaces are designed servos 9B89 for work which involved gasifier 9D153. Power of all systems of the missile is provided turbogenerator 9D154.
Thrust front - 14820 kg
Hours RDTT maximum - 70
-------------
Engine missile 9M714 . The numbers denote: 1 - Mechanical part of the case solid propellant rocket motors, 2 - a charge of fuel, 3 - cylindrical shell, 4 - valve, 5 - hoop-buckle, 6 - posterior part of the solid propellant rocket motors; 7 - rotating nozzle, 8 - Mechanical part of the body SRBs, 9 - the main bulwark of solid propellant rocket motors, 10 - primer, 11 - cover, 12 and 13 - Thermal protection;
--
---------
Nozzle engine block OTR 9M714 "Oka at the exhibition IDET-1994
In front of the missile unit installed engine brake used for braking rocket unit in the department of warheads
--
--------
Brake rocket engine 9M714
--
--
Length:
- 7520 mm (9M714, 9M714K - on questionable data)
- 7315 mm (9M714K)
- 7516 mm (9M714B, 9M714UT)
The length of the block without a missile warheads - 5170 mm
Diameter - 974 mm
A swing-open lattice rudders - 1848 mm
Weight:
- 4400-4690 kg
- 4630 kg (9M714K)
- 4400 kg (9M714B)
- 4480 kg (9M714B1)
Weight without warheads - 3990 kg
Warhead weight - 372-715 kg
Weight-cone adapter to connect the unit with rocket warheads - 80 kg
Range:
- 50 km (minimum, 9M714)
- 300 km (9M714K)
- 400 km (9M714B, according TTX)
- 407-450 km (maximum 9M714, depending on the type of warhead, but 9M714K)
- 500 km (Oka-U, up to 700 km stage design)
The height of the top point of the trajectory - 120 km
The rocket's velocity at the end of the active region of the trajectory - 4 M
Speed warheads in the final stage - 10 M
CEP:
- 50-150 m (Oka, 350 m from dr.dannym)
- 30 m (Oka-U)
Hours charge elektroturbogeneratora missiles - with 97,5
Deployment time from march - 5 minutes (?)
Time ready for launch in March - 3 min
Lifting time rocket from the transport situation in the starter - 20 p.
Time replacement warheads on the STC - 15 minutes
Time guaranteed storage - 10 years
Time to guarantee the storage in the field - 3 years
=======================
Warhead: according to the media in the development of warheads we considered the radar visibility. Form warheads and the center of gravity provide aerodynamic stabilization of warheads in the terminal phase of flight. To compensate for the mass of the nuclear charge, which in size is in the widest part of the cone warhead, in the bow of Warhead is compensating for the load. Warhead was combined with missile launch unit through a transitional compartment, which have different types of warheads different. In the case of nuclear warheads in the transitional compartment located (as of mid-1980's) cutting foil, self-opening spring reflectors, compact sources of active interference and false Warhead (simulator Warhead). The transfer module was mounted with the warheads at the manufacturing plant and separately in the troops is not available. The design of the transfer compartment nuclear warheads 9B513 differs from the construction of other types of transfer compartment warheads. When you create a set of missiles and envisaged the possibility of promotion warheads after separation from the carrier in order to improve accuracy. In the transitional compartment of nuclear warheads is perpendicular to the axis of products are two engine promotion, but to the control system are not connected and not used in production because Warhead in the process of testing to improve the accuracy of warheads has not happened.
- Cluster 9N74K (missile 9M714K) with cluster munitions 9N224 involving a 95 explosive submunitions 9N225 (weight - 3,84 kg explosive weight - 0,64 kg, dimensions - 328 x 64 mm, forms the 300 fragments weighing 5 g), central charge 9H313 (sometimes written 9CH313), combined fuse 9A253, the appliance division bomblets 9CH59, backup fuse 9A133, 9B246 electric battery (voltage of 28.5 volts) and altimeter 9A333-1. Transport and storage was carried out in a container 9YA251. Cluster Warhead for export may not bear means to overcome missile defense, and probably equipped with high-explosive submunitions 9N225.
On arms of the USSR Supreme Council consisted 9K714K missiles with warheads 9N74K Markets homing-shaped high explosive submunitions, which are in the air rotate around its axis in the search for the mass of metal. If you are approaching the land mass of metal was found, then the low-altitude engine fires, directing the sub-munition to the target, which is affected cumulative jet. If the target is not detected, it is undermining the combat element when hitting the ground like conventional high-explosive fragmentation munition. If the fuse when hitting the ground is not successful, then after some time triggered fuze self-destruct
Length - 2755 mm
Diameter - 800 mm
Weight - 716 lbs
Mass container 9YA251 - 1297 kg
Height undermine - 3000 m
Hours electric batteries Warhead - 430 with
Activation time of electric battery Warhead - not more than 16
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Cassette Warhead 9N74K (size and weight model) in a container 9YA251 on trolley 9T114
-
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9N74K before the destruction of warheads, Czech Republic, 1993
- Nuclear 9N74B (rocket 9M714B) with a capacity of 10-50 kilotons. Transport and storage was carried out in a container 9YA252. Warhead is connected to the missile transfer compartment 9B513.
Warhead weight - 375 kg.
- Thermonuclear 9N63 (missile 9M714B1) with the charge of the AA-75 200 kiloton (according to the museum VNIIEF, Sarov). Transport and storage was carried out in a container 9YA252. Warhead is connected to the missile transfer compartment 9B513.
Warhead weight - 375 kg.
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Launch 9M714B1 with teaching and training Warhead 9N63UT. Photo of the annex to the Treaty on the Reduction of INF (1987). In the mistaken view of Western analysts rocket in the photo is equipped with a penetrating conventional warheads.
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Thermonuclear Warhead OTR Oka Museum RFNC-VNIIEFg. Sarov
- Blast 9N74F (rocket 9M714F) with penetrating abilities (Western data).
- Chemical warheads (according to Western data).
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=======================
Warhead: according to the media in the development of warheads we considered the radar visibility. Form warheads and the center of gravity provide aerodynamic stabilization of warheads in the terminal phase of flight. To compensate for the mass of the nuclear charge, which in size is in the widest part of the cone warhead, in the bow of Warhead is compensating for the load. Warhead was combined with missile launch unit through a transitional compartment, which have different types of warheads different. In the case of nuclear warheads in the transitional compartment located (as of mid-1980's) cutting foil, self-opening spring reflectors, compact sources of active interference and false Warhead (simulator Warhead). The transfer module was mounted with the warheads at the manufacturing plant and separately in the troops is not available. The design of the transfer compartment nuclear warheads 9B513 differs from the construction of other types of transfer compartment warheads. When you create a set of missiles and envisaged the possibility of promotion warheads after separation from the carrier in order to improve accuracy. In the transitional compartment of nuclear warheads is perpendicular to the axis of products are two engine promotion, but to the control system are not connected and not used in production because Warhead in the process of testing to improve the accuracy of warheads has not happened.
- Cluster 9N74K (missile 9M714K) with cluster munitions 9N224 involving a 95 explosive submunitions 9N225 (weight - 3,84 kg explosive weight - 0,64 kg, dimensions - 328 x 64 mm, forms the 300 fragments weighing 5 g), central charge 9H313 (sometimes written 9CH313), combined fuse 9A253, the appliance division bomblets 9CH59, backup fuse 9A133, 9B246 electric battery (voltage of 28.5 volts) and altimeter 9A333-1. Transport and storage was carried out in a container 9YA251. Cluster Warhead for export may not bear means to overcome missile defense, and probably equipped with high-explosive submunitions 9N225.
On arms of the USSR Supreme Council consisted 9K714K missiles with warheads 9N74K Markets homing-shaped high explosive submunitions, which are in the air rotate around its axis in the search for the mass of metal. If you are approaching the land mass of metal was found, then the low-altitude engine fires, directing the sub-munition to the target, which is affected cumulative jet. If the target is not detected, it is undermining the combat element when hitting the ground like conventional high-explosive fragmentation munition. If the fuse when hitting the ground is not successful, then after some time triggered fuze self-destruct
Length - 2755 mm
Diameter - 800 mm
Weight - 716 lbs
Mass container 9YA251 - 1297 kg
Height undermine - 3000 m
Hours electric batteries Warhead - 430 with
Activation time of electric battery Warhead - not more than 16
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Cassette Warhead 9N74K (size and weight model) in a container 9YA251 on trolley 9T114
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9N74K before the destruction of warheads, Czech Republic, 1993
- Nuclear 9N74B (rocket 9M714B) with a capacity of 10-50 kilotons. Transport and storage was carried out in a container 9YA252. Warhead is connected to the missile transfer compartment 9B513.
Warhead weight - 375 kg.
- Thermonuclear 9N63 (missile 9M714B1) with the charge of the AA-75 200 kiloton (according to the museum VNIIEF, Sarov). Transport and storage was carried out in a container 9YA252. Warhead is connected to the missile transfer compartment 9B513.
Warhead weight - 375 kg.
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Launch 9M714B1 with teaching and training Warhead 9N63UT. Photo of the annex to the Treaty on the Reduction of INF (1987). In the mistaken view of Western analysts rocket in the photo is equipped with a penetrating conventional warheads.
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Thermonuclear Warhead OTR Oka Museum RFNC-VNIIEFg. Sarov
- Blast 9N74F (rocket 9M714F) with penetrating abilities (Western data).
- Chemical warheads (according to Western data).
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The composition of the complex equipment OTR 9K714 Oka:
- STC 9P71;
- TZM 9T230;
- Transport vehicle 9T240 - combination with a truck ZIL-131. Warheads and missile components were transported in containers:
- - 9YA249 - Missile part without warheads;
- - 9YA251 - cluster warheads;
- - 9YA252 - special (nuclear) warheads;
- Checkout machine 9V69;
- Training kit 9F633;
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STC 9P71
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TZM 9T230 (official picture of the documentation to the Treaty on the Reduction of INF, 1987)
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TZM 9T230 army Slovakia
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Transport vehicle 9T240 with a missile 9M714
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Transport vehicle 9T240 with a missile 9M714
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Scheme device transport vehicles 9T2
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Capping missile unit in the container for transport 9YA249 car 9T240 (top) and the container 9YA251 (bottom). Army Slovakia
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Containers for the missile unit 9YA249 (left) and for nuclear warheads 9YA252 (right). Фото с http://www.rwd-mb3.de/ .
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Checkout machine 9V69 rocket unit 9M714 on lodgement. Foreground Warhead 9M74K and container 9YA251
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Checkout machine 9V69
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The composition of the complex equipment OTR 9K714 Oka:
- STC 9P71;
- TZM 9T230;
- Transport vehicle 9T240 - combination with a truck ZIL-131. Warheads and missile components were transported in containers:
- - 9YA249 - Missile part without warheads;
- - 9YA251 - cluster warheads;
- - 9YA252 - special (nuclear) warheads;
- Checkout machine 9V69;
- Training kit 9F633;
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STC 9P71
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TZM 9T230 (official picture of the documentation to the Treaty on the Reduction of INF, 1987)
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TZM 9T230 army Slovakia
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Transport vehicle 9T240 with a missile 9M714
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Transport vehicle 9T240 with a missile 9M714
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Scheme device transport vehicles 9T2
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Capping missile unit in the container for transport 9YA249 car 9T240 (top) and the container 9YA251 (bottom). Army Slovakia
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Containers for the missile unit 9YA249 (left) and for nuclear warheads 9YA252 (right). Фото с http://www.rwd-mb3.de/ .
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Checkout machine 9V69 rocket unit 9M714 on lodgement. Foreground Warhead 9M74K and container 9YA251
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Checkout machine 9V69
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Modifications:
Complex 9K714 Oka, missile 9M714 (1976) - serial missile base unit.
9M714F rocket - the rocket with explosive and / or with penetrating warheads;
Launch 9M714K - missile with cluster warheads;
Launch 9M714B - missiles with nuclear warheads;
Rocket 9M714B1 - rocket with thermonuclear warheads;
Launch 9M714GVM - size and weight model rockets, visually different lattice control surfaces with diagonal cross-shaped ridges.
Launch 9M714UT - training missiles, visually distinguished by the size of the reduced lattice control surfaces and other structures of the nozzle block missiles
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Launch 9M714GVM (size and weight model
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Trainer missile 9M714UT at STC 9P71 Army Slovakia
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Modifications:
Complex 9K714 Oka, missile 9M714 (1976) - serial missile base unit.
9M714F rocket - the rocket with explosive and / or with penetrating warheads;
Launch 9M714K - missile with cluster warheads;
Launch 9M714B - missiles with nuclear warheads;
Rocket 9M714B1 - rocket with thermonuclear warheads;
Launch 9M714GVM - size and weight model rockets, visually different lattice control surfaces with diagonal cross-shaped ridges.
Launch 9M714UT - training missiles, visually distinguished by the size of the reduced lattice control surfaces and other structures of the nozzle block missiles
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Launch 9M714GVM (size and weight model
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Trainer missile 9M714UT at STC 9P71 Army Slovakia
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Complex 9K714U Oka-U, rocket 9M714U - KY-19 (1987) - GRAU supposedly upgraded version of the R & D began in 1982 and MSC TSNIIAG. It was supposed to adopt a new set of weapons to replace the tactical Oka. The missile was equipped with guided warhead with aerodynamic control surfaces and radar homing. According to unconfirmed reports provided redirected range missiles in flight. It was supposed to use missiles as part of a reconnaissance and strike systems in conjunction with aircraft reconnaissance and target designation M-55 Mystic-B. The tests at 1987 were conducted. The complex was to be launched in series production. After the conclusion of the INF Treaty on the Reduction of planned R & D to reduce the range of the "Oka-U, to refine the homing systems and adopt a set of arms.
"Sphere" / "Field-M" (1991) - project geophysical rocket-based missile Oka and Oka-V ", first shown in March 1993 on one of the aerospace exhibitions.
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Model rocket "Sphere-M is developed on the basis of tactical Oka-U
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Complex 9K714U Oka-U, rocket 9M714U - KY-19 (1987) - GRAU supposedly upgraded version of the R & D began in 1982 and MSC TSNIIAG. It was supposed to adopt a new set of weapons to replace the tactical Oka. The missile was equipped with guided warhead with aerodynamic control surfaces and radar homing. According to unconfirmed reports provided redirected range missiles in flight. It was supposed to use missiles as part of a reconnaissance and strike systems in conjunction with aircraft reconnaissance and target designation M-55 Mystic-B. The tests at 1987 were conducted. The complex was to be launched in series production. After the conclusion of the INF Treaty on the Reduction of planned R & D to reduce the range of the "Oka-U, to refine the homing systems and adopt a set of arms.
"Sphere" / "Field-M" (1991) - project geophysical rocket-based missile Oka and Oka-V ", first shown in March 1993 on one of the aerospace exhibitions.
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Model rocket "Sphere-M is developed on the basis of tactical Oka-U
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In some media meets the following system of kinds of NATO:
Launch 9M714B - SS-23 SPIDER-A
Launch 9M714F - SS-23 SPIDER-B
Launch 9M714K - SS-23 SPIDER-C
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Scheme TZM 9T230 。
The numbers denote: 1 - the panel of external cladding 2 - latching mechanism, and 3 - to send the selection of engine power, 4 - valve, 5 - tool boxes, 6 - Traverse 9T320; 7 - Universal traverse 9T319 8 - power support; 9 - marching mount , 10 - chassis 14 - navigation system TNA-4, 15 - hydraulic drive, 16 - engine housing TZM; 17 - thermally insulated container, rocket warheads, 18 - electric generator, 19 - rotating mechanism crane, 20 - electrical equipment; 21 - boom Crane, 22 - support; 23 - ZIP, 24 - bandages (slings) 9YA251; 25 - compensator; 26 - a single set of spare parts; 27 - prop rocket;
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Projections STC 9P71 complex 9K714 Oka. Camouflage - the top - the USSR, 1985, at the bottom - export "eastern" version, 1985 Drawing from the book Zaloga Steven J., The SCUD and other Russian Ballistic Missile Vehicles. Concord Publication
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Status:
USSR:
- 1979 - the beginning of mass production. By 1987 inclusively produced 106 STCs and 88 TZM.
- 1980 - Adopting a and supplies to the troops.
- 1985 - accommodation in the GDR (GSVG) 75 STC (Western data).
- 1987 December - a total production of the STC and TZM industry over the years - 106 STCs and 88 TZM. The deployment of tactical "Oka" in the armed forces (training missiles were not considered):
Part GSVG - 16 STC, 53 armed missiles;
Part of the USSR - 66 STC, 114 operational missiles;
Warehouses of the USSR Supreme - 13 STC, 33 operational missiles (SPU - pos.Berezovka, missiles - pos.Ladushkin). 36 STC and 72 missiles at dr.dannym (not confirmed).
Training centers of the USSR Supreme - 7 SPU (Saratov, Kazan, Kamenka).
TOTAL: 102 STC, 200 combat missiles.
1987 December 7 - stopped training on complex 9K714 Oka VVUZah in the USSR.
- 1987-1988 GG - A set of "Oka" was in service with the following parts of the USSR Armed Forces (the full range of missile armed with 6 teams (trehpolkovogo composition) and a separate missile regiment):
- 189 th Missile Brigade (p.Stankovo), in 1985, rearmed in the missile 9K714 Oka, Belarusian IN (18 STC).
- 233rd Missile Brigade (p.Slobudka Brest region), in 1985, rearmed in the missile 9K714 Oka, Belarusian IN (18 SPU);
- 199 Guards Missile Brigade (1985 rearmed on missile 9K714 Oka); disbanded 21/03/1989 g, Belarusian IN (18 STC).
- One orbr in GSVG (12 SPU);
- One orbr in Kazakhstan-Turkmenistan (12 SPU);
- One PFU (regiment) in GSVG (4 STC).
1989 - fully reduced (102 STCs and 208 missiles). According to Steven Zaloga - 106 STCs and 239 missiles.
In some media meets the following system of kinds of NATO:
Launch 9M714B - SS-23 SPIDER-A
Launch 9M714F - SS-23 SPIDER-B
Launch 9M714K - SS-23 SPIDER-C
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Scheme TZM 9T230 。
The numbers denote: 1 - the panel of external cladding 2 - latching mechanism, and 3 - to send the selection of engine power, 4 - valve, 5 - tool boxes, 6 - Traverse 9T320; 7 - Universal traverse 9T319 8 - power support; 9 - marching mount , 10 - chassis 14 - navigation system TNA-4, 15 - hydraulic drive, 16 - engine housing TZM; 17 - thermally insulated container, rocket warheads, 18 - electric generator, 19 - rotating mechanism crane, 20 - electrical equipment; 21 - boom Crane, 22 - support; 23 - ZIP, 24 - bandages (slings) 9YA251; 25 - compensator; 26 - a single set of spare parts; 27 - prop rocket;
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Projections STC 9P71 complex 9K714 Oka. Camouflage - the top - the USSR, 1985, at the bottom - export "eastern" version, 1985 Drawing from the book Zaloga Steven J., The SCUD and other Russian Ballistic Missile Vehicles. Concord Publication
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Status:
USSR:
- 1979 - the beginning of mass production. By 1987 inclusively produced 106 STCs and 88 TZM.
- 1980 - Adopting a and supplies to the troops.
- 1985 - accommodation in the GDR (GSVG) 75 STC (Western data).
- 1987 December - a total production of the STC and TZM industry over the years - 106 STCs and 88 TZM. The deployment of tactical "Oka" in the armed forces (training missiles were not considered):
Part GSVG - 16 STC, 53 armed missiles;
Part of the USSR - 66 STC, 114 operational missiles;
Warehouses of the USSR Supreme - 13 STC, 33 operational missiles (SPU - pos.Berezovka, missiles - pos.Ladushkin). 36 STC and 72 missiles at dr.dannym (not confirmed).
Training centers of the USSR Supreme - 7 SPU (Saratov, Kazan, Kamenka).
TOTAL: 102 STC, 200 combat missiles.
1987 December 7 - stopped training on complex 9K714 Oka VVUZah in the USSR.
- 1987-1988 GG - A set of "Oka" was in service with the following parts of the USSR Armed Forces (the full range of missile armed with 6 teams (trehpolkovogo composition) and a separate missile regiment):
- 189 th Missile Brigade (p.Stankovo), in 1985, rearmed in the missile 9K714 Oka, Belarusian IN (18 STC).
- 233rd Missile Brigade (p.Slobudka Brest region), in 1985, rearmed in the missile 9K714 Oka, Belarusian IN (18 SPU);
- 199 Guards Missile Brigade (1985 rearmed on missile 9K714 Oka); disbanded 21/03/1989 g, Belarusian IN (18 STC).
- One orbr in GSVG (12 SPU);
- One orbr in Kazakhstan-Turkmenistan (12 SPU);
- One PFU (regiment) in GSVG (4 STC).
1989 - fully reduced (102 STCs and 208 missiles). According to Steven Zaloga - 106 STCs and 239 missiles.
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One of the episodes of the destruction of missiles "Oka" method of detonation. Warhead - education. Sary-Ozeki, approximately 1989
1993 March - MSC proposed to the development of geophysical complex "Sphere" with missiles of "Oka".
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Monument Complex 9K714 Oka at Kapustin Yar (http://kapyar.ru)
Export:
Bulgaria:
- 1985-1988 GG - Put 4 STC (from other sources - 8 SPU) and 18 missiles 9M714K.
- 1997 - according to official figures armed with 8 complexes (or 4 STC and 4 TZM?)
- 2000 - is in service.
- 2001 December - are reduced.
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STC complex 9K714 Oka Museum in Sofia (Bulgaria, file photo Carrey, http://russianarms.ru)
GDR:
- 1985-1988 GG - Put 4 STC and 18 missiles 9M714K. Operated by the 5-th Missile Brigade NVA DDR (g.Demen).
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TZM 9T230 (left) and SPU 9P71 (right) of the National People's Army of the GDR
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Complex 9K714 with size and weight dummy missiles 9M714GVM missile brigade of the National People's Army of the GDR
- 1990 March - cut, destroyed dismantling. Battle of the, apparently, by the explosion.
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Dismantling STC complex 9K714 Oka in the GDR, 15 March 1990
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The destruction of missiles and cluster warheads 9N74K complex 9K714 in the GDR, March 1990
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Romania:
- 1987-1988 GG - 1987-1988 GG - put 4 STC and 18 missiles 9M714K. - Put 4 STC and 18 missiles 9M714K.
- 2002 - there is evidence that reduced. - 2002 - there is evidence that reduced.
Syria - 1987-1989 GG Syria - 1987-1989 GG - scheduled deliveries to the conclusion of the Treaty on the Reduction of INF. - Planned delivery to the conclusion of the Treaty on the Reduction of INF.
Czechoslovakia: Czechoslovakia:
- 1985-1988 GG - 1985-1988 GG - put 4 STC and 18 missiles 9M714K. After the dissolution of Czechoslovakia remained in Slovakia (5 th missile regiment, g.Martin). - Put 4 STC and 18 missiles 9M714K. After the dissolution of Czechoslovakia remained in Slovakia (5 th missile regiment, g.Martin).
- 1993 - Czech destroyed by dismantling some of the complexes or missiles are stored. - 1993 - in the Czech Republic destroyed by dismantling some of the complexes or missiles are stored.
- 1996 - armed with 4 STC and 18 missiles 9M714K. - 1996 - armed with 4 STC and 18 missiles 9M714K.
- 2002 - rocket destroyed (Slovakia) - in accordance with the memorandum signed with the United States for compensation in the amount of 16 million. - 2002 - rocket destroyed (Slovakia) - in accordance with the memorandum signed with the United States for compensation in the amount of 16 million. Disassembly was carried out in Trencin. Disassembly was carried out in Trencin.
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One of the episodes of the destruction of missiles "Oka" method of detonation. Warhead - education. Sary-Ozeki, approximately 1989
1993 March - MSC proposed to the development of geophysical complex "Sphere" with missiles of "Oka".
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Monument Complex 9K714 Oka at Kapustin Yar (http://kapyar.ru)
Export:
Bulgaria:
- 1985-1988 GG - Put 4 STC (from other sources - 8 SPU) and 18 missiles 9M714K.
- 1997 - according to official figures armed with 8 complexes (or 4 STC and 4 TZM?)
- 2000 - is in service.
- 2001 December - are reduced.
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STC complex 9K714 Oka Museum in Sofia (Bulgaria, file photo Carrey, http://russianarms.ru)
GDR:
- 1985-1988 GG - Put 4 STC and 18 missiles 9M714K. Operated by the 5-th Missile Brigade NVA DDR (g.Demen).
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TZM 9T230 (left) and SPU 9P71 (right) of the National People's Army of the GDR
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Complex 9K714 with size and weight dummy missiles 9M714GVM missile brigade of the National People's Army of the GDR
- 1990 March - cut, destroyed dismantling. Battle of the, apparently, by the explosion.
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Dismantling STC complex 9K714 Oka in the GDR, 15 March 1990
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The destruction of missiles and cluster warheads 9N74K complex 9K714 in the GDR, March 1990
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Romania:
- 1987-1988 GG - 1987-1988 GG - put 4 STC and 18 missiles 9M714K. - Put 4 STC and 18 missiles 9M714K.
- 2002 - there is evidence that reduced. - 2002 - there is evidence that reduced.
Syria - 1987-1989 GG Syria - 1987-1989 GG - scheduled deliveries to the conclusion of the Treaty on the Reduction of INF. - Planned delivery to the conclusion of the Treaty on the Reduction of INF.
Czechoslovakia: Czechoslovakia:
- 1985-1988 GG - 1985-1988 GG - put 4 STC and 18 missiles 9M714K. After the dissolution of Czechoslovakia remained in Slovakia (5 th missile regiment, g.Martin). - Put 4 STC and 18 missiles 9M714K. After the dissolution of Czechoslovakia remained in Slovakia (5 th missile regiment, g.Martin).
- 1993 - Czech destroyed by dismantling some of the complexes or missiles are stored. - 1993 - in the Czech Republic destroyed by dismantling some of the complexes or missiles are stored.
- 1996 - armed with 4 STC and 18 missiles 9M714K. - 1996 - armed with 4 STC and 18 missiles 9M714K.
- 2002 - rocket destroyed (Slovakia) - in accordance with the memorandum signed with the United States for compensation in the amount of 16 million. - 2002 - rocket destroyed (Slovakia) - in accordance with the memorandum signed with the United States for compensation in the amount of 16 million. Disassembly was carried out in Trencin. Disassembly was carried out in Trencin.
新浪网不会从这里再拿图片吧.............:D
lz你终于又出来了，祝贺啊！[:a15:]
回复 29# JSTCVW09CD
在这里冒头了呀，快去科普俺的帖子。
在这里冒头了呀，快去科普俺的帖子。