F-22A Raptor Sukhoi Flanker F-111 Aardvark F/A-18A Hornet Joint Strike Fighter Weapons Aerial Refuelling and Airlift Issues ISR and NCW Issues Regional Capability Issues Defence Policy and Reform Issues Supporting Air Power in Australia
  Directed Energy Weapons and Electromagnetic Bombs Systems and Basic Technology Australia's First Online Journal Covering Air Power Issues [ISSN 1832-2433] Information Warfare, Information Operations and Electronic Attack Air Power and National Military Strategy Issues

Last Updated: Sun May 18 10:25:37 UTC 2008


Russian Low Band Surveillance Radars
(Counter Low Observable Technology Radars)

Nebo SVU VHF AESA Analysis [Click for more ...]

S-300 SAM System Analysis [Click for more ...]




  September, 2007
Updated April, 2008
by Dr Carlo Kopp
© 2007 Carlo Kopp

(Images Rosoboronexport, RuMoD, NNIIRT, US DoD, Other)

 

The Northrop-Grumman B-2A 'Batwing' is sufficiently large that its shaping remains effective against lower band radars. The same is not true for fighters with LO shaping (US DoD).

Background:

Prior to the rout of Saddam's extensive IADS in the 1991 Desert Storm campaign, the Soviets did not take US stealth technology seriously. Desert Storm changed that entirely, and the Soviets launched an effort to develop capabilities to detect VLO aircraft. With the collapse of the USSR funding dried up, but Russian design bureaus including NNIIRT, well known for their line of P-18 Spoon Rest VHF band radars, continued developing new systems operating in the lower bands - from VHF through UHF to L-band.

Most stealth design features are intended to scatter incoming illumination in a controlled fashion, evidenced by the use of edge alignment, faceting and other geometrical shaping features, supplemented by the use of absorbent materials. All of these techniques are intended to defeat radars operating in the geometrical optics and less frequently, resonance regimes of scattering. The precondition for this to work is that the wavelength be much shorter than the cardinal dimensions of the shaping feature of interest. An edge aligned engine inlet of typical dimensions will perform best in the centimetric Ku- and X-bands, and less so with increasing radar wavelength.

The Russian approach has been to invest in the further development of low band radars, especially operating in the VHF band. With wavelengths of the order of a metre or more, only very large stealth aircraft (eg B-2A) satisfy the physics requirement for geometrical optics regime scattering. A fighter sized aircraft such as the JSF will see most of its carefully designed shaping features fall into the resonance or Raleigh scattering regions, where shaping is of little or no import, and skin depth penetration of the induced electrical surface currents defeats most absorbent coatings or laminates.



The physics of radar scattering depend to a large extent on the size of the radar wavelength vs the physical size of the target. In the Raleigh scattering regime, the wavelength is similar or greater in magnitude to the physical size of the target, and the magnitude of the reflection is essentially proportional to the physical size of the target. As the wavelength is reduced, the resonant region is entered, where the wavelength is comparable in size to key shaping features on the target, and the magnitude of the reflection fluctuates strongly with wavelength and aspect. Finally, in the optical scattering regime, target shaping can be used to precisely control the magnitude and direction of reflections. The high effectiveness of stealth designs against decimetric and centimetric band radars reflects the reality that for most aircraft sizes, these wavelengths are a tenth to a hundredth of the size of key shaping features (Author).

Low band radars are not a panacea for the defeat of VLO (Very Low Observable) aircraft. Their angular accuracy has been until recently poor, and the required antenna size results in ungainly systems which are usually slow to deploy and stow, even if designed from the outset for mobility. The size and high power emissions of these radars, in types with limited mobility, makes them much easier to detect and destroy than typical mobile systems operating in the decimetric and centimetric bands, which can relocate rapidly after a missile shot.

Despite these drawbacks, the older Russian low band radars still provide a valuable early warning capability, and enable cueing of other sensors and platforms. In an IADS context, a 55Zh6 Nebo, 1L13 Nebo SV, Nebo SVU or 5N84 Oborona would be used to cue the high power aperture X-band 30N6E Flap Lid series and 9S32M Grill Pan series engagement radars in the S-300PMU, S-400/S-400M and S-300VM systems to a small acquisition box in which the VLO aircraft can be found. This allows signficantly more RF power to be focussed into a small volume of space, increasing the probability of detection. Some newer radars such as the Nebo SVU are accurate enough to direct a missile shot, using the engagement radar primarily as a midcourse command/datalink channel to the missile.

Where fighters with high power aperture X-band radars are available, such as Irbis-E or Zhuk ASE equipped Su-30/35 Flanker E/G/H variants, a low band radar can provide GCI vectors to position the fighter near enough for acquisition of the target, if need be with other sensors such as an IR Search and Track set.


US DoD Band Allocation Chart

In practical terms one of the key advantages of VLO aircraft, surprise, is largely denied by the use of such systems. The VLO capability is still enormously valuable in terms of degrading or defeating most engagement radars and missile seekers, but the defender regains access to the early phases of the engagement cycle otherwise also defeated by VLO capability.

The US Air Force is expected to use the F-22A Raptor armed with the glide wing equipped GBU-39/B SDB to destroy a defender's low band systems in the opening minutes of an engagement, relying on the standoff range of the weapon and speed/altitude of the fighter to deny engagement opportunities by defending IADS elements being cued by the low band radars. Other fighters do not have these capabilities and become exposed to defending IADS elements.

The notion that Russian low band radars are artifacts of the Cold War with little combat value is foolish, as current production models are typically 'digitised' through most of the signal and data processing, and display components, and many now use solid state transmitters. At least one designs is an AESA (active phased array). Russian manufacturers have thus followed much the same trend as Western manufacturers, enhancing Cold War era systems designs with digital processing. More than often modern Digital Moving Target Indicator (DMTI) or digital pulse Doppler techniques are employed, exploiting the high performance of COTS computing technology, readily available in the open market and easy to ruggedise for a semi-mobile application of this kind.

Russian industry is very actively marketing digital upgrades to the P-18 Spoon Rest, and new production digital 55Zh6 Nebo UE / Tall Rack and Nebo SVU VHF radars, specifically as a "Counter-Stealth" capability.





While the JSF is frequently criticised for the limitations of its stealth capability in the mid and upper microwave bands, the compact size of this aircraft makes it highly susceptible to detection by low band radars, unlike larger aircraft such as the B-2A Spirit (US Air Force).
 




Resources:

Нижегородский научно-исследовательский институт радиотехники' (ННИИРТ), Россия, 603950, Нижний Новгород, ул. Шапошникова, 5, тел. (+78312) 65-00-69, факс (+78312) 64-02-83
Eugene Yanko - Warfare.ru - Russian Air Defence Radars


55ж6-1 Небо-УЕ Трехкоординатная РЛС дежурного режима
55Zh6-1 Nebo UYe / Tall Rack 3-Dimensional Surveillance Radar





(Images via NNIIRT)





1Л13-3 Небо СВ Двухкоординатная РЛС дежурного режима
1L13-3 Nebo SV 2-Dimensional Surveillance Radar





 





Additional Images (1) and (2) Here (Images via NNIIRT)





1Л119 Небо СВУ  МОБИЛЬНАЯ Трехкоординатная РЛС дежурного режима
1L119 Nebo SVU Mobile 3-Dimensional Surveillance Radar

Nebo SVU VHF AESA Analysis [Click for more ...]



The new Nebo SVU AESA is an improved new technology derivative of the baseline 1L13 Nebo SV series of VHF radars. It has an array of 84 (14 x 6) vertically polarised VHF Yagis, unlike the 72 elements in the 1L13, each with a 3/8 folded dipole and director element. Unlike the 1L13 carried by a Ural 4320 6x6 truck, the larger Nebo SV is a semi-trailer arrangement towed by a Ural 4320 tractor.



The fully digital Nebo SVU is a solid state VHF band surveillance radar intended for the detection of airborne and ballistic targets. These include tactical and bomber aircraft, and low altitude and stealth aircraft targets. Capabilities include an integrated IFF array and the ability to track airborne noise jammers. Key features include:
  1. Active phased array antenna (AESA) design with a Transmit Receive Modules integrated with each of the antenna elements, analogue-to-digital conversion of each channel, with the option of digital beamforming in the vertical plane for ABM operating modes.
  2. Fully digital signal processing.
  3. Adaptive automatic operation to handle countermeasures and antenna element failures.
  4. Digital processing designed to handle adverse weather and intensive chaff bombing.
  5. Adaptive sidelobe cancellation.
  6. Heightfinding capability.
  7. Very high 500 hour MTBF compared to legacy VHF radars, as a result of the AESA technology used.
A key consideration when assessing the Nebo SVU is its greater mobility compared to other VHF radars. The Ural 4320 towed trailer arrangement has similar cross country and road mobility to the KrAZ-260 towed variants of the S-300PMU/S-400 TEL. More importantly, the ~20 minute deployment and stow times are much improved over earlier VHF radars in this class, more than twofold compared to the P-18 Spoon Rest or Nebo SV, and threefold over the legacy S-300PMU acquisition radar, the 36D6 Tin Shield. Currently the most mobile Russian acquisition radar is the 64N6E series ESA, towed by a MAZ-543 derived tractor, and capable of "shoot and scoot" operations with times of minutes. We should not be surprised to see future variants of the Nebo SVU equipped with more advanced stow/deploy mechanisms to emulate the "shoot and scoot" capabilities of the 64N6E series.

What has not been disclosed about the Nebo SVU is the specific mechanism used for high precision angle tracking, it is likely that high speed electronic sequential lobing is employed to emulate amplitude monopulse techniques. Details of the active sidelobe cancellation and jammer nulling mechanisms have also not been disclosed. While reports have emerged of the integration of the 55Zh6 Nebo UE with the S-400 C3 system, none have been seen as yet on the integration of the Nebo SVU.



Basic Characteristics
Waveband
metric
Upper limits of detection range and target coordinate measurement:



In altitude, km
No less than 100 in search mode; no less than 180 in tracking mode



In elevation, deg
No less than 25 in search mode; no less than 45-50 in tracking mode

Detection range for aircraft and ballistic targets with RCS of 1 m2, km:




at 0.5 km altitude, km
65
at 10 km altitude, km
270
at 20 km altitude, km
380
Measurement Accuracy:

range, m
200
azimuth, arcmin
30
elevation angle, arcmin
1.5 (within 3 to 45 deg elevation angle range)

Ouput data format
tracks
Number
 of individual
 targets tracked

100
Data update rate, s
10 and 5
MTBF, hr

at least 500
MTTR, hr
0.5
Crew, personnel
4 (single )
Number of vehicles
2
Deployment time, min
20
Power consumption, kW
30
Основные характеристики:

Диапазон волн
метровый
Верхняя граница зоны обнаружения и измерения координат:

по высоте, км
не менее 100 – в режиме регулярного кругового обзора; не менее 180 – в режиме досопровождения
по углу места, град.
не менее 25 – в режиме регулярного кругового обзора; 45-50 – в режиме досопровождения
Дальность обнаружения аэродинамических и баллистических целей с ЭОП 1м2, км:

на высоте 0,5 км
65
на высоте 10 км
270
на высоте 20 км
380
Точность измерения координат:

дальности, м
200
азимута, мин.
30
угла места, мин.
1,5 (в диапазоне углов места от 3 до 45 град.)
Вид выходной информации
трассы
Количеств
о одновременно сопровождаемых целей
100
Темп обновления информации, с
10 и 5
Среднее время наработки на отказ, ч
не менее 500
Среднее время восстановления, ч
0,5
Обслуживающий персонал, чел.
4 (в одну смену)
Количество транспортных единиц
2
Время развертывания, мин.
20
Энергопотребление, кВт
30





CETC JY-27 VHF Band Long Range Surveillance Radar




The CETC JY-27 is a recent Chinese design which is clearly influenced by the 1L13 Nebo SV and 1L119 Nebo SVU. Yet to be validated open source specifications are:

Detection range (Pd = 0.8,  Pf = 0.000001, σ = 1.5 m²) [NMI]
240.0 - 390.0
Frequency  Band VHF
Array Geometry
16 x 6 = 96 elements H-pol
Bandwidth Δ f 15% of  carrier frequency
Detection accuracy - Range
±150m
Detection accuracy - Azimuth
±1º
Mainlobe width
MTI Clutter rejection [dB]
35.0
MTBF [hr]
MTTR [hr]
>250.0
0.5
Power Consumption [kW]
<50.0

The radar is claimed to provide pseudorandom frequency hopping, and ECCM capabilities. The absence of elevation error specs suggests the radar lacks a height finding capability. All images to date show a towed installation. The very sparse brochure claims the radar is 'fully solid state' but no further details have been disclosed.



МОБИЛЬНАЯ ДВУХКООРДИНАТНАЯ РАДИОЛОКАЦИОННАЯ СТАНЦИЯ
МЕТРОВОГО ДИАПАЗОНА ВОЛН П-18-2
P-18-2/P-18M 
Spoon Rest D/E Mobile 2-Dimensional Metric Band Surveillance Radar



P-18 Spoon Rest (Hungarian MoD)





NNIIRT modernised P-18 Spoon Rest (NNIIRT)



NITEL
modernised P-18 Spoon Rest (NITEL).



ПОДВИЖНАЯ ДВУХКООРДИНАТНАЯ  РАДИОЛОКАЦИОННАЯ СТАНЦИЯ
МЕТРОВОГО ДИАПАЗОНА ВОЛН 
НИТЕЛ 5Н84АЭ «ОБОРОНА-14» (1РЛ113/44Ж6/5Н84)
NITEL 5N84AE Oborona-14 / Tall King C Mobile 2-Dimensional
Metric Band
Surveillance Radar






Stowed Configuration Image (1) Here.

(Images via http://forum.valka.cz/)





РАДИОЛОКАЦИОННАЯ СТАНЦИЯ «ГАММА-ДЕ»

67N6E GAMMA-DE  Mobile 3-Dimensional Solid-State Phased Array Surveillance Radar



Stowed Configuration Image (1) Here.






РАДИОЛОКАЦИОННАЯ СТАНЦИЯ
51У6/39Н6Э «КАСТА-2Е1» / «КАСТА-2Е2» /
П-15 /
П-15M / П-19
51U6/39N6E Kasta 2E1/2E2 /
P-15 / P-15M / P-19
Flat Face E / Squat Eye E Surveillance Radar



Kasta 2E1 Flat Face E UHF Acquisition Radar.





Kasta 2E2 Squat Eye E





P-15 Flat Face







Stowed Configuration Images (1) and (2) Here.



P-19 Flat Face.




1L13 Nebo SV



F-22A Raptor Sukhoi Flanker F-111 Aardvark F/A-18A Hornet Joint Strike Fighter Weapons Aerial Refuelling and Airlift Issues ISR and NCW Issues Regional Capability Issues Defence Policy and Reform Issues Supporting Air Power in Australia
  Directed Energy Weapons and Electromagnetic Bombs Systems and Basic Technology Australia's First Online Journal Covering Air Power Issues [ISSN 1832-2433] Information Warfare, Information Operations and Electronic Attack Air Power and National Military Strategy Issues
Artwork, graphic design and text © 2004, 2005, 2006, 2007 Carlo Kopp; Text © 2004, 2005, 2006, 2007 Peter Goon; All rights reserved.
Recommended browsers Mozilla/Firefox, Konqueror.
$Revision: 1.327 $
NLA Pandora Archive
Notices