![]() |
||||||||||||||||||||||||||||||||||||||||||
|
||||||||||||||||||||||||||||||||||||||||||
| ||||||||||||||||||||||||||||||||||||||||||
|
NIEMI/Antey
9K81/9K81-1/9K81M
Self Propelled Air Defence System / SA-12/SA-23 Giant/Gladiator НИЭМИ/Антей Cамоходный Зенитный Ракетный Комплекс 9К81/9К81-1/9К81М / Антей 2500 Technical Report APA-TR-2006-1202 |
||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
| by
Dr Carlo Kopp, SMAIAA, MIEEE, PEng First published 2003 Updated December 2006 Updated August 2007 Updated June, December 2008 Updated July 2009 Text, Line Art © 2003-2009 Carlo Kopp |
||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
![]() The S-300V/S-300VM/Antey-2500 is the world's only truly mobile Anti Ballistic Missile system, and later variants are claimed to be capable of intercepting 4.5 km/sec reentry speed targets. The large size of the Grill Pan phased array and TELAR command link and illuminator antennas is evident. The system provides the capability to engage very low RCS aircraft at ranges in excess of 100 nautical miles. Below: 9M82 Giant round (images © Miroslav Gyűrösi). ![]() |
||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
|
||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
Background
|
||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
![]() Novator 9M82 / SA-12B Giant and 9M83 / SA-12A Gladiator Surface to Air MissilesThe two stage 9M83 / SA-12A
Gladiator
and 9M82 / SA-12B Giant are the guided missiles used by the S-300V /
SA-12 system. The missiles are largely common in design, the principal
distinctions being different first stage boosters, and different
control surface arrangements.
The smaller 9M83 Gladiator
SAM/ABM is intended to engage aerial targets at all altitudes,
including
cruise missiles, and smaller TBMs. The much larger 9M82 Giant has
higher kinematic performance and is intended to kill IRBMs, SRAM class
supersonic missiles, but also standoff jamming aircraft at long ranges.
Both weapons employ two solid propellant stages, with thrust vector control of the first stage (10,225 lb/4,636 kg mass in the Giant and cca 5,000 lb/2275 kg in the Gladiator) and aerodynamic control of the 2,800 lb (1,200 kg) second stage, using four servo driven fins, and four fixed stabilisers. The guidance and control packages, and much of the weapon airframes are identical, the principal distinction being the bigger booster stage of the Giant and its larger stabilisers. A cold start ejector is used to
expel the missile from the launch tube, the first stage burns for about
20 seconds, upon which the missile transitions to its midcourse
sustainer. During midcourse flight the
missile employs inertial
navigation with the option of command link updates. In the former mode
it transitions to its semi-active homing seeker during the final 10
seconds of flight, in the latter 3 seconds before impact - a technique
preferred for heavy jamming environments. Russian sources claim the semi-active seeker can lock on to a 0.05 square metre RCS target from 16.2 nautical miles. The midcourse guidance system attempts to fly the most energy efficient trajectory to maximise range. A two channel radio proximity fuse is used to initiate the 330 lb (150 kg) class “smart” warhead which has a controllable fragmentation pattern to maximise effect. The engagement envelope of the baseline Gladiator is between 80 ft AGL to 80 kft, and ranges of 3.2 to 40 nautical miles, the Giant between 3,200 ft AGL to 100 kft, and ranges of 7 to 54 nautical miles. The system can launch the missiles at 1.5 second intervals, and a battalion with four batteries can engage 24 targets concurrently, with 2 missiles per target, and has a complement of between 96 and 192 missiles available for launch on TELAR/TELs. A TELAR can arm a missile for launch in 15 seconds, with a 40 second time to prepare a TELAR for an engagement, and 5 minute deploy and stow times - a genuine shoot and scoot capability. The cited single shot kill probabilities for the Gladiator are 50% to 65% against TBMs and 70% to 90% against aircraft, for the Giant 40% to 60% against IRBMs and 50% to 70% against the AGM-69 SRAM - ballistic missiles with re-entry velocities of up to 3 km/s can be engaged. The Soviets were terrified of
TAC's EF-111A force and equipped the
S-300V system with a facility for passive targeting of support jammers.
The 9S15, 9S19 and 9S32 have receiver channels for sidelobe jamming
cancellation and these are used to produce very accurate bearings to
the airborne jammer, this bearing information is then used to develop
angular tracks. The angular tracks are then processed by the 9S457
command post to estimate range, and the 9S32 then develops an estimated
track for the target jammer. A Giant missile is then launched and
steered by command link until it acquires the target.
![]() 9M82
Giant round and 9Ya238 transport container.
![]() 9M83 Gladiator round and 9Ya240 transport container. ![]() 9M82
Giant round nozzle detail.
![]()
9M83 Gladiator round nozzle detail.
|
||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
Production and Exports
|
||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
![]() |
![]() |
Like the S-300P series systems, the S-300V
uses the cold launch technique, ejecting the missile before its motor
is fired. These 9M83 SAMs are being launched from a 9A83 TELAR, which
uses its elevated directional antenna to provide the 9M83 with both
midcourse command updates and terminal phase high power continuous wave
illumination of the target. Antey claim the semi-active seeker will
acquire a 0.05 square metre RCS target at 16 nautical miles
(Rosvooruzheniye).
|
|
| Основные
характеристики ЗРС С-300В Principal Characteristics of the S-300V SAM System |
|||
| Зона
поражения аэродинамических целей, км Engagement Envelope for Aircraft Targets [km] |
|||
| - по дальности - in range |
до 100
|
||
| - по высоте - in altitude |
0,025...30
|
||
| Зона поражения
баллистических целей по высоте, км Engagement envelope for ballistic missile targets in altitude [km] |
1...25
|
||
| Максимальная
скорость поражаемых целей, м/с Maximum velocity of defeated targets [m/s] |
3000
|
||
| Число целей,
одновременно обстреливаемых дивизионом Number of targets concurrently engaged by a single battery |
24
|
||
| Число ЗУР,
одновременно наводимых дивизионом Number of SAMs, concurrently guided by battery |
24
|
||
| Темп стрельбы, с Rate of fire [sec-1] |
1,5
|
||
| Время подготовки
ЗУР к пуску, с Time to prepare SAM for launch [sec] |
15
|
||
| Время перевода
системы из дежурного режима в боевой, с Time to transition system from standby mode to operational mode [sec] |
40
|
||
| Боекомплект ЗУР
дивизиона (на ПУ и пускозаряжающих установках) Single battery missile count (on TELARs and TEL/Transloaders) |
96-192
|
||
| Вероятность
поражения ракеты "Ланс" одной ЗУР 9М83 9M83 Gladiator Single Shot Pk [-] vs Lance TBM |
0,5...0,65
|
||
| Вероятность
поражения самолета одной ЗУР 9М83 9M83 Gladiator Single Shot Pk [-] vs aircraft target |
0,7...0,9
|
||
| Вероятность
поражения головной части ракеты "Першинг" одной ЗУР 9М82 9M82 Giant Single Shot Pk [-] vs Pershing RV |
0,4...0,6
|
||
| Вероятность
поражения ракеты СРЭМ одной ЗУР 9М82 9M82 Giant Single Shot Pk [-] vs AGM-69A SRAM |
0,5...0,7
|
||
| Основные
характеристики ЗУР системы
С-300В Principal Characteristics of the S-300V SAMs |
||
| Наименование Designation |
9М83 / SA-12A Gladiator
|
9М82 / SA-12B Giant
|
| Длина, мм Length [mm] |
7898 (8570)
|
9913 (10525)
|
| Максимальный диаметр, мм Maximum diameter [mm] |
915 (930)
|
1215 (1460)
|
| Масса, кг: Mass [kg]: |
3500 (3600)
|
5800 (6000)
|
| - первой ступени - first stage |
2275
|
4635
|
| - второй ступени - second stage |
1213
|
1271
|
| Масса боевой части, кг Warhead Mass [kg] |
150
|
н/д
N/A |
| Средняя скорость полета,
м/с Average flight velocity [m/s] |
1200
|
1800
|
| Максимальная перегрузка,
ед. Maximum load factor [G] |
20
|
20
|
| Границы зоны
эффективного действия, км Engagement Envelope [km] |
||
| - дальняя - maximum range |
75
|
100
|
| - верхняя - maximum altitude |
25
|
30
|
| - ближняя - minimum range |
6
|
13
|
| - нижняя - minimum altitude |
0,025
|
1
|
| Потенциальная дальность
захвата ГСН цели с ЭПР 0,05 кв.м Seeker acquisition range for target with 0.05 m2 RCS [km] |
30
|
30
|
| 9K81
Battery Components |
|||
| System |
Qty |
Function/Composition |
Vehicle |
| 9S32
Grill Pan |
1 |
Self Propelled Engagement Radar | GM-833 |
| 9A82
(SA-12B) |
2 |
Transporter
Erector Launcher And Radar |
GM-830 |
| 9A84 (SA-12B) | 1 |
Transporter
Erector Launcher /
Transloader |
GM-834 |
| 9A83 (SA-12A) | 4 |
Transporter Erector Launcher And Radar | GM-831 |
| 9A85 (SA-12A) | 2 |
Transporter Erector Launcher / Transloader | GM-835 |
| 9T82 | 2 | Missile Reload Transporter | |
| 9T83 | 2 | Missile Reload Transporter | |
| 9T447-1 |
2 |
Missile
Reload Transporter |
|
| 9T325 |
1 |
Missile
Rigging Station |
Ural-43203-1012 |
| 9В868-1/1R15 |
1 |
Equipment Repair/Test Station | Ural-43203-1012 |
| 9В898-1/1R16 |
1 |
Equipment
Repair Station |
Ural-43203-1012 |
| 9V878-1 |
1 |
Equipment Repair Station | Ural-43203-1012 |
| 9V879-1 |
1 |
Equipment Repair Station | Ural-43203-1012 |
| 9V91 |
1 |
Mobile
Automatic Test Station |
ZIL-131 |
| 9V927 | 1 | Mobile Automatic Test Station | ZIL-131 |
| PES-100T/400-AKP1 |
1 |
Mobile
Power Generator |
- |
| UKS-400V |
1 |
Mobile
Air Compressor |
- |
| AGZ-M1 |
1 |
Mobile
Workshop |
- |
| 9F88 |
1 |
Training
Simulator |
- |
| 9M82UR/UD,
9M83UR/UD |
1+1 |
Training
Round, Cutaway Training Round |
- |
| 9M82/9M83 |
24-48 |
Missile
Reloads |
- |
| 9K81
Battalion Components (4 Batteries) |
|||
| 9S457 | 1 | Self Propelled Command Post | GM-837 |
| 9S15MT
Obzor 3 / Bill Board |
1 | Self Propelled Acquisition Radar | GM-832
|
| 9S19M2
High Screen |
1 | Self Propelled ABM Acquisition Radar | GM-836 |

9A82
TELAR deployed (Image © Miroslav Gyűrösi).


9A83
TELAR deployed (Image © Miroslav Gyűrösi).

9A83 TELAR stowed (Image © Miroslav Gyűrösi).




9A83
TELAR Stowed.



9A83 TELAR Deployment.






|
||||||||||||||||||
| ||||||||||||||||||