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

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September, 2007
Updated April, 2008
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by
Dr Carlo Kopp
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| ©
2007 Carlo Kopp |
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(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).
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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).

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

(Images via NNIIRT)

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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:
- 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.
- Fully digital signal processing.
- Adaptive automatic operation to handle countermeasures and
antenna element failures.
- Digital processing designed to handle adverse weather and
intensive chaff bombing.
- Adaptive sidelobe cancellation.
- Heightfinding capability.
- 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.
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Basic
Characteristics
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Waveband
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metric
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Upper
limits of detection range and target coordinate measurement:
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In
altitude, km
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No
less than 100 in
search mode; no less than 180 in tracking mode
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In
elevation, deg
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No
less than 25 in
search mode; no less than 45-50 in tracking mode
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Detection range for aircraft and ballistic
targets with RCS of 1 m2, km:
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at
0.5
km altitude, km
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65
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at
10
km altitude, km
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270
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at
20
km altitude, km
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380
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Measurement Accuracy:
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range,
m
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200 |
azimuth,
arcmin
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30 |
elevation
angle, arcmin
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1.5
(within 3 to 45 deg elevation angle range)
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Ouput
data format
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tracks
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Number
of individual
targets tracked
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100
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Data
update rate, s
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10
and
5
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MTBF,
hr
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at
least 500
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MTTR,
hr
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0.5
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Crew,
personnel
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4
(single )
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Number
of vehicles
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2
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Deployment
time, min
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20
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Power
consumption, kW
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30
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Основные характеристики:
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Диапазон
волн
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метровый
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Верхняя
граница зоны обнаружения и измерения координат:
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по
высоте, км
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не
менее 100 – в режиме регулярного кругового обзора; не менее 180 – в
режиме досопровождения
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по
углу места, град.
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не
менее 25 – в режиме регулярного кругового обзора; 45-50 – в режиме
досопровождения
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Дальность обнаружения аэродинамических и
баллистических целей с ЭОП 1м2, км:
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на
высоте 0,5 км
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65
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на
высоте 10 км
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270
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на
высоте 20 км
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380
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Точность измерения координат:
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дальности,
м
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200
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азимута,
мин.
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30
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угла
места, мин.
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1,5
(в диапазоне углов места от 3 до 45 град.)
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Вид
выходной информации
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трассы
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Количеств
о одновременно сопровождаемых целей
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100
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Темп
обновления информации, с
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10
и 5
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Среднее
время наработки на отказ, ч
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не
менее 500
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Среднее
время восстановления, ч
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0,5
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Обслуживающий
персонал, чел.
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4
(в одну смену)
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Количество
транспортных единиц
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2
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Время
развертывания, мин.
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20
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Энергопотребление,
кВт
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30
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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]
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240.0 - 390.0
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| Frequency
Band |
VHF
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Array
Geometry
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16 x 6 = 96
elements H-pol
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| Bandwidth
Δ f |
15% of
carrier frequency
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Detection
accuracy - Range
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±150m
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Detection
accuracy - Azimuth
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±1º
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Mainlobe
width
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7º |
MTI
Clutter rejection [dB]
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35.0
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MTBF
[hr]
MTTR [hr]
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>250.0
0.5
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Power
Consumption [kW]
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<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.
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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).
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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/)

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РАДИОЛОКАЦИОННАЯ СТАНЦИЯ «ГАММА-ДЕ»
67N6E GAMMA-DE Mobile 3-Dimensional Solid-State Phased Array Surveillance Radar

Stowed
Configuration Image (1) Here.

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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
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Artwork, graphic design and text © 2004, 2005, 2006, 2007 Carlo Kopp; Text © 2004, 2005, 2006, 2007 Peter Goon; All
rights reserved. |
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