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TRANSCRIPT
Moscow, 2013
High sensitivity GaAs photocathode technology designed for using in night vision goggles GEO-NVG1 offers significant mprovement in low – light viewing The implementation of more reliable and affordable Third generation image intensiver Tubes provides
GEO-N VG1 with maximum performance and reliability at starlight overcast light level
Features III Generation IIT TechnologyFull binocular night visionErgonomic and EstheticRugged and Compact Design Qualified to Russian Military RequirementsAllow Full Peripheral Vision
Five – Position RotaryQuick DisconnectCan be Adapter to StandartAviator HelmetComfortable in usingAutomatic Brightness ControlInternal Power Supply
Third generation Aviators night Vision Goggles GEO-NVG1-01
ApplicationNap-of-earth flyingBorder patrol and securityCovert observation and night combat Search and rescue Reconnaissance
Image intensifier tube gen III:
System specification:
Photocathode Type GaAs Scene illumination 5 x10-4 lux ÷ 0.1 lux
Photocathode Sensitivity
1500 μA/lm Magnification 1*
Radiant (λ=830 nm) 150 mA/W Field of View 38° (min)
Gain 25000 Exit Pupil 8 mm
Signal/Noise Ratio E=10-4 lux
17 Resolution 23 mm
Center Resolution 45 mm-1 Resolution 0,65 cy/mrad
Useful Cathode Diameter
17,5 mm Objective lens 25 mm
Input faceplate Glass, Ñ57 Aperture 1/1,2
Output Faceplate Fiber Optics Inverter
Eyepiece Lens 25 mm
Dimension ∅ 36,75 mm x 31 mm
Voltage required 27 V DC 50mA
Power source Helicopter electricalwiring system
Battery 2 AA size Alkaline (316)
Weight 540 grams
Mechanical adjustment range:
Vertical 16 mm
Fore & Aft 24 mm
Interpupillary Eyepiece
54 ÷ 72 mm
Diopter +2D -4D
Теchnical characteristics
The Aviator’s Night Vision Goggles (NVG) «GEO-NVG1- 01» provide the crew with an opportunity of viewing the terrain at night (illumination range
5•10-4 ÷ 10-1 lux) and realization of the following action:
takeoff; hovering; flying at heights from 50 up to
200 m with the visual control of a terrain; - approach and execution of landings with a contact of ground on the nonequipped
and not covered platforms. All military Russian helicopter pilots now benefit from the ergonomic end technological enhancements incorporated into «GEO-NVG1-01» goggles.
High sensitivity GaAs photocathode technology designedfor using in night vision goggles offers significantimprovement in low – light viewingThe implementation of more reliable and affordable Third GenerationImage Intensifier Tubes (IIT Gen. III) provides with maximumperformance and reliability at starlight overcast light level.The objective lenses utilize the integrated minus-blue filter which is compatible withhelicopter equipped green-yellow-red cockpit lightings.
ApplicationNap-of-earth flyingBorder patrol and securityCovert observation and nightcombatSearch and rescueReconnaissance
FeaturesIII Generation IIT TechnologyFull binocular night visionErgonomic and EstheticRugged and Compact DesignQualified to Russian MilitaryRequirementsAllow Full Peripheral Vision
Five – Position RotaryQuick DisconnectCan be Adapter to StandardAviator HelmetComfortable in usingAutomatic BrightnessControlInternal Power Supply
Third generation Aviators night Vision Goggles GEO-NVG1-01
Image intensifier tube gen III:
System specification:
Photocathode Type GaAs Scene illumination 5 x10-4 lux ÷ 0.1 lux
Photocathode Sensitivity 1500 μA/lm Magnification 1*
Radiant (λ=830 nm) 150 mA/W Field of View 40°
Gain 25000-45000 Exit Pupil 8 mm
Signal/Noise Ratio E=10-4 lux
20 Eye relief 23 mm
Center Resolution 50 mm-1 System distortion Less than 2 %
Useful Cathode Diameter
17,5 mm Resolution 0,65 cy/mrad
Input faceplate Glass, C57 Focal length 25 mm
Output Faceplate Fiber Optics Inverter
F Number 1,2
Dimension ∅ 36,75 mm x 31 mm
Input voltage 27 volts DC
Input currant 50 mA
Power source Helicopter electricalwiring system
Battery voltage 2 AA size Alkaline(316),
2.0 to 3.0 volts DC
Weight 550 grams
Mechanical:Vertical 16 mm
Fore & Aft 24 mm
Interpupillary Eyepiece
54 ÷ 72 mm
Diopter +2D to -4D
Теchnical characteristics
The Aviator’s Night Vision Goggles (NVG) GEO-NV - III -NVG provide the crew with an opportunity of viewing the terrain at night (illumination range 5•10-4 ÷ 10-1 lux) and
realization of the following action: takeoff;
hovering; approach and execution of landings with a contact of ground on the non equipped
and not covered platforms. High sensitivity GaAs photocathode technology designed for using in night vision
goggles offers significant improvement in low – light viewing
The implementation of more reliable and affordableThird Generation Image Intensifier Tubes (IIT Gen. III) provides with maximum performance and reliability at starlight overcast light level. The objective lenses utilize the integrated minus-blue filter which is compatible with helicopter equipped green-yellow-red cockpit lightings.
AplicationNap-of-earth flyingSearch and rescueReconnaissance
FeaturesIII Generation IIT TechnologyFull binocular night visionErgonomic and EstheticRugged and Compact DesignQuick Disconnect
Can be Adapter toStandard Aviator HelmetComfortable in usingAutomatic BrightnessControlInternal Power Supply
Third generation night Vision Goggles GEO-NV - III - NVG
Image intensifier tube gen III:
System specification:
Photocathode Type GaAs Scene illumination
5 x10-4 lux ÷ 0.1 lux
Photocathode Sensitivity
1300 μA/lm Magnification 1*
Radiant (λ=830 nm) 130 mA/W Field of View 38°
Gain 25000 Exit Pupil 8 mm
Signal/Noise Ratio E=10-4 lux
17 Eye relief 23 mm
Center Resolution 36 mm-1 System distortion Less than 2 %
Useful Cathode Diameter
17,5 mm Resolution 0,65 cy/mrad
Input faceplate Glass, C57 Focal length 25 mm
Output Faceplate Fiber Optics Inverter
F Number 1,2
Dimension ∅ 36,75 mm x 31 mm
Input voltage 27 volts DC
Input currant 50 mA
Power source Helicopter electricalwiring system
Battery voltage 2 AA size Alkaline(316),2.0 to 3.0 volts DC
Weight 550 grams
Mechanical:Vertical 16 mm
Fore & Aft 24 mm
Tilt adjustment 10 0
Interpupillary Eyepiece
52 ÷ 72 mm
Diopter +2D to -4D
Теchnical characteristics
Теchnical characteristics
Supervision out of cabin spaceand helicopter pilotage at nightwith maintenance of indication flightparameters of movement, position inspace and the additional information.Helicopter take off and landing on notequipped platforms in night conditions.Searching people and technics.Covert flight of helicopters at night.High quality image in natural night light conditionsby application of III-rd generation IIT allowing toimprove vision in low light level conditions considerably.Comfortable vision in NVG is provided by high qualityeyepieces, great value of output diameters and their disposalfrom design elements.Simple moving in not-working position.Possibility to use independent power sources.SYSTEM FEATURESStereoscopic vision in a wide angular field.Convenient fastening on a protective helmet and individual regulation for operator’s eyes,realized by four mounts.Ergonomic indication of additional parameters provided by application of OLED microdisplay.Manual brightness control of additional parameters
Aviators night vision goggles with micro display for flightparameters visualization GEO-NVG1-VI
Main characteristics: Mechanical characteristics:Scene illumination 5·10-4-0,1 lx Adjustment range
Magnification 1 * Diopter +2 ÷ -2 dptr
Field of view 38 ° Interpupillary Eyepiece
54 - 72 mm
Exit pupil 12 mm Vertical 16 mm
Eye relief 23 mm Horisontal 24 mm
Resolution 1,0 cycle/mrad
Focal length 26 mm
Aperture 1:1,2
Required Voltage 27 V (50 mА)
Weight 730 g
Теchnical characteristics
IIT characteristics:Photocathode typeSensitivity:
GaAs
- Light 1500 μА/lm
- radiant (830 nm) 150 mА/W
EBI 6·10-11 lx
Signal/Noise ratio (Е=10-4 lx) 17
Photocathode diameter 17,5 mm
Resolution 45 mm-1
Input faceplate Glass С-57
Output faceplateInverter fiber-
opticsElement
Dimensions ∅ 36, 75-31 mm
Image Intensifer Tubes IIIGeneration IIT 217G IIT 204G
Теchnical characteristics
PERFOMANCE CHARACTERISTICS
IIT 217 G with usefuldiameter 25 mm
IIT 204 G with usefuldiameter 25 mm
min min
Photocathode Sensitivitya
Luminous (2854OK) μA/Im 1200 1800
Radiant (λ = 830 nm) mA/W 100 180
Luminous Gain (1-5) x 10 -4 lux 25000 35000
Background brightness cd/m 3*10-3 3*10-3
Signal-to-Noise Ratio (E=10-4 lux) 15 15
Center Resolution lp/mm 36 36
Output Background cd/m2 3-8 3-8
Modulator transfer function, %
2,5 Lp/mm7,5 Lp/mm15,0 Lp/mm
0,850,600,38
0,860,580,28
Weight, g 150 150
PHOTOCATHODE
Type of photocatocathode GaAs GaAs
Spectral Range 450 ÷ 930 530 ÷ 930
nput optics Glass, C-57 Glass, C-57
Cathode Diameter, mm ∅ 25 ∅ 25
PHOSFOR SCREEN
Type KC-527 KC-527
Image output Inverter Inverter
Dimension, mm ∅ 64 x 22 ∅ 64 x 22
Image Intensifer TubesIII Generation IIT 58G IIT 218G
Теchnical characteristics
PERFOMANCE CHARACTERISTICSIIT 58G-01 with
usefuldiameter 18 mm
IIT 58G-01 with usefuldiameter 18 mm
min max min
Photocathode Sensitivitya
Luminous (2854OK) μA/Im 1300 1600 1800
Radiant (λ = 830 nm) mA/W 120 150 180
Luminous Gain (1-5) x 10 -4 lux 25000 35000 35000
Background brightness cd/m 3*10-3 3*10-3
Signal-to-Noise Ratio (E=10-4 lux) 16 18 25
Center Resolution lp/mm 40 45 50
Output Background cd/m2 3-8 3-8 3-8
Modulator transfer function, %2,5 Lp/mm7,5 Lp/mm15,0 Lp/mm
0,860,640,35
0,900,700,45
Weight, g 85 85
PHOTOCATHODE
Type of photocatocathode GaAs GaAs
Spectral Range 530 ÷ 930
530 ÷ 930
Input optics Glass, C-57
Glass, C-57
Cathode Diameter, mm ∅ 17.5 ∅ 18 ∅ 17.5
PHOSFOR SCREEN
Type KC-527 KC-527
Image output Inverter Inverter
Dimension, mm ∅ 36,7x31 ∅ 36,7x31
Photosensitive modules, consisted of III generation image intensifier tubes with negative electron
affinity photocathode, coupled with CCD matrix intended for night vision
TV systems. All of four modules is working in
next spectral ranges: PSM V-IR - 0,5-0,9 μm; PSM UV - 0,2-0,35 μm;
PSM IR1 - 0,4-1,1 μm; PSM IR2 - 0,95-1,65 μm.
Photosensitive modules on base of imageintensifier tubes III generation
All modules have on output standard TV signal - 1V 75Om.
Resistance to environment conditions GOST RM
20.39.414.1
Теchnical characteristics
PERFOMANCE CHARACTERISTICS PSM V-IR PSM UV PSM IR1 PSM IR2
Spectral range Μm 0,5-0,9 0,2-0,35 0,4-1,1 0,95-1,65
Sensitivity:
- Light μA/lm 2500 - 400 -
- radiant (850 nm) mA/W 220 - 50 -
- radiant (1060 nm) mA/W - - 2,5 -
Work TV resolution Tvl 450 400 400 450
Signal/Noise ratio (E-10-4 lx) 20 - 9 -
Power supply (voltage) V 12 12 12 12
Power supply (current) mA 250 250 250 250
Output frame format Pixel 768x576 768x576 768x576 768x576
Digital capacity of output signal Bit 12 12 12 12
Threshold irradiance W/m2 - 5 10-7 - -
Work irradiance W/m2 - 5 10-4 - -
Quantum efficiency (1540 nm) % - - - 2
FILTERS are intended for adaptation aircraft interior lighting
compatible with Aviator’s Night Vision Goggles (NVG)
using Third Generation Image intensifier Tubes (IIT Gen. III) for providing flight at day and night time (with or without NVG) at different Natural illuminance
levels. FILTERS are intended for adaptation aircraft interior lighting compatible with Aviator’s Night Vision
Goggles (NVG) using Third Generation Image Intensifier Tubes (IIT Gen. III) for ensure operation aircraft
compatible lighting with NVG rage at night time at low-light-level. FILTERS are designed to meet all the requirements of Russian standard & International standard MIL-STD-3009.
OVERALL PERFORMANCE
Adaptation of aircraft interior lighting is substitution of standard (red) lightfilters on adapted (compatible with NVG) color (green, yellow and red) FILTERS immediately in consoles, panels, instrument and display panel lighting and etc.FILTERS can be quantified with any reference source. SPU «Geophisika» supplies filter data with the actual source specified by customers application.Brightness adjustment of the aircraft interior lighting compatible with NVG is carried out the assistance of voltage control, allowing to adjust a voltage of a power supply of lampsfrom 10 V up to 27 V.
Aircraft Filters Compatiblewith Night Vision Goggles
Теchnical characteristics
FILTERS color Green Yellow Red
Photo optical transmission coefficient 16% 19% 17%
Chromaticity CIE’76
U’ 0,14 0,27 0,4
V’ 0,57 0,56 0,54
Color temperature 2000 K 2000 K 2000 K
NVIS RADIANCE, w/(sr•sm2) Less 1,7x10-11 Less 1,5x10-8 Less 1,4x10-7
IR sources are intended for the installation in the exterior lighting systems. They provide
a safe single and group flying of helicopters in the night with the NVG system used only. The guidance is done at the various levels of night light exposure on a terrain. IR sources
work in a Covert mode. In this mode supervision of lights from outside and in the limited distances is provided by using a NVG. Unaided detection of the lights is excluded.
All IR sources represent a tactical replaceable complete set which is subject
to installation for performance of special tasks. IR sources are a NVG
compatible Infra-Red replacement for wing and tail, formation and blade
screwing light bulbs. They provide a simple economical means of temporarily
converting visible lights to IR for covet operations. Remove the incandescent
lamps, insert IR sources and modification is complete.
IR sources are equipped with the current stabilization system, which is
particularly useful in case of ambient environment temperature changes.
IR Sources for the Exterior Lighting Systems inNVG Compatible Helicopter
Теchnical characteristics
IR Source TypeГЕО-ИИС-
014ГЕО-ИИС-
013ГЕО-ИИС-
015ГЕО-ИИС-
017ГЕО-ИИС-
016
Exterior Lighting Type FormationОПС-57
Tail tipXC-62
Tail tipXC-39 Wing tip
БАНО-64
Light blades of
thebearing screwМи-8
АМТ/МТВ
Supply Operating Voltage(24-28) V DC
(5-8) RMSAC 400 Hz
Nominal Operating Voltage, B 27 VDC
7,5 RMSAC 400 Hz
Current by Nominal OperatingVoltage
11 mA 8 mA 8 mA 15 mA 15 mA
Peak Emission Wavelength (905 ± 5) nm
IR Output Radiation on axis) 1,5 W/sr 1 W/sr 1 W/sr 2 W/sr 1,5 W/sr
IR Sources Specification:
Light sources are intended for installation in the exterior lighting system. The sources
provide secure both single and formation day-night piloting of helicopters. Piloting is feasible both with and without usage of
the NVG under different terrain lighting levels.
Light sources work in “Visible NVG friendly” mode, which provides visual supervision with a naked eye. It doesn’t diminish the distance of NVG action and
reduces visibility of lights for a considerably distant observer with NVG.
Setting the light sources on the board the helicopter:doesn’t require changes in mounting dimensionsof used Exterior lighting system. Light sources are fullyinterchangeable with the incandescent lamps;requires changing the nominals of ballast resistors, controllingthe mode “bright/dull”;supposes the presence adaptation of helicopter’s cockpit for using NVG.Light sources are equipped with the current stabilization system, which is particularlyuseful in case of ambient environment temperature changes.Light sources are created for the usage in the items ОПС– 57, ХС – 62, ХС – 39,БАНО – 64, МСЛ - 3 – 2с, lights of rotor blade. They satisfy the requirements of RussianFederation standard and MIL - STD – 3009. Such products with established light sourcesconform to the requirements of international aviation rules FAR p.29.Light sources withstand all types of environmental exposures for the light sources of theexternal lightening system.
IR sources for an Exterior Lighting Systems inNVG Compatible Helicopter
Теchnical characteristics
Light source Type ГЕО-ИИА-001 ГЕО-ИИА-001 ГЕО-ИИА-005 ГЕО-ИИА-007
Exterior Lighting Type FormationОПС-57 Tail tip XC-62 Tail tip XC-39 Wing tip
БАНО-64
Supply Operating Voltage 10-32 V DC
Nominal Operating Voltage 27 V DC
Current by Nominal OperatingVoltage
150 mА 300 mА 150 mА 600 mА
Colour in Exterior Lighting Typeof by FAR p.29
Yellow / Green Aviation white
Aviation white
Aviation green,
Aviation red
Luminous intensity on axis 10 cd 27 cd 10 cd 100 cd
NVIS radiance,for brightness 50 cd/m2
10-6 /3·10-7
W/(sr sm⋅ 2)10-6
W/(sr sm⋅ 2)10-6
W/(sr sm⋅ 2)3·10-7
W/(sr sm⋅ 2)
Light source Type ГЕО-ИИА-011 ГЕО-ИИА-012 ГЕО-ИИА-002 ГЕО-ИИА-010
Exterior Lighting Type Anti collisionlights
МСЛ-3-2c
Light blades of
Ка-52Light blades of
Ми-8АМТLight blades
ofМи-8АМТВ
Supply Operating Voltage 18-31 V DC 5-8 RMS AC 400 Hz
Nominal Operating Voltage 27 V DC 7,5-8 RMS AC 400 Hz
Current by Nominal OperatingVoltage
650 mА 65 mА 200 mА 200 mА
Colour in Exterior Lighting Typeof by FAR p.29
Aviation red Aviation white Aviation whiteAviation
white
Luminous intensity on axis effective 400 cd 3,5 cd 5 cd 5 cd
NVIS radiance,for brightness 50 cd/m2
3·10-7
W/(sr sm⋅ 2)10-6
W/(sr sm⋅ 2) 10-6 W/(sr sm⋅ 2) 10-6 W/(sr sm⋅ 2)
Dual mode radiation sources are intended for installation into the exterior
lighting system. Piloting is feasible both with and without usage of
the NVG under different terrain lighting levels. Dual mode radiation sources work in “Visible NVG Friendly” mode with an opportunity of switching the “Covert” mode. This construction doesn’t have analogues for all over the world. “Visible NVG friendly” mode provides visual supervision with a naked eye. It doesn’t diminish the distance of NVG action and reduces visibility of lights for a considerably distant
observer with NVG. “Covert” mode provides supervision of lights from outside in the limited distances, which eliminates the
unaided detection of the lights. Detection by considerably distant observer with NVG is impossible.Setting the dual mode sources on the board the helicopter :
doesn’t require changes in connecting sizes of used lights. Dualmode sources are fully interchangeable with used incandescent lamp;
requires changing the nominal and scheme of switching the ballast resistors,controlling the mode “bright/dull” and changing the selector for “bright/dull” to“ bright /dull/covert ”;supposes the presence adaptation of helicopter’s cockpit for using NVG.Dual mode radiation sources have integrated current stabilization system from the raised temperature of the environment. They satisfy the requirements of Russian Federation standard and MIL STD - 3009. Such products with established dual mode sources conform to the requirements of international aviation rules FAR p.29.
Dual mode radiation sources are equipped with the current stabilization system, which is particularly useful in case of ambient environment temperature changes.
Emitting sources withstand all types of environmental exposures for the light sources of the external lightening system.Installation of such sources in a heluopter turns it into a moltipurpose “nigpe” lighting complex.
IR sources for an Exterior Lighting Systems inNVG Compatible Helicopter
Теchnical characteristics
Dual mode radiation source Type ГЕО-ИИД-018 ГЕО-ИИД-018
Exterior Lighting Type Formation ОПС-57 Total tip ХС-62
In “Visible NVG friendly” mode
Supply Operating Voltage 10-32 V DC
Nominal Operating Voltage 27 V DC
Current by Nominal Operating Voltage 150 mА 300 mА
Colour in Exterior Lighting Type of by FAR p.29 Yellow Aviation white
Luminous intensity on axis 10 cd 27 cd
NVIS radiance, for brightness 50 cd/m2 10-6 W/(sr sm⋅ 2) 10-6 W/(sr sm⋅ 2)
In “Covert” mode
Supply Operating Voltage 5,5-7,5 RMS AC 400 Hz
Current by Operating Voltage 6 V 11 mA 8 mA
Peak Emission Wavelength 905±5 nm
Radiant Intensity on axis 1,5 W/sr 1 W/sr
General descriptions of IR- sources:
Night and Day TV camera for helicopterssighting system consists of low-level TV system and Day TV channel. GEO-NTK4 is derived on base of Third Generation Image Intensifier Tube (IIT Gen. III.) coupled with digital CCD camera. Third Generation Image Intensifier Tube consists of: GaAs photocathode; Micro channel
Plate (MCP) and Phosphor screen. GEO-NTK4 has the Day channel, which provides automatic transfer from night to day
Regime by the video signal level control.
GEO-NTK4 has a special digital processor for image enhancement
Opportunity to use the unguided weapon at day & night time.
High technology recognition & low cost.
Augmented operating range at the expense of usage IR spectral range & digital
processing of the “Night” & “Day” imagery.Detection & recognition targets on the AMLCD.
Night & Day TV Camera Gyro stabilized System forHelicopters GEO-NTK4
Technical specification: Image intensifier tube Gen. III:
Configuration Night TV cameraDay TV camera Photocathode type GaAs
Television standard 625 TV lines, 25 Hz
Photocathode sensitivity:
TV dissector Horizontal, across-line Luminous 1800 μA/lm
Power consumption 12 W, 0,5 A Radiant 180 mA/W
Temperature ofexploitation +50°C ÷ -40°C EBI 3x10-3 cd/m2
Weight: Gain 30000
Night TV camera 1,7 kg Signal/Noise ratio (E=10-4 lux) 20
Day TV camera 0,7 kg Illumination range (10-5÷10-1) lux
Dimensions: Photocathode diameter 24,5 mm
Night TV camera 225 x 87 x 90 mm Resolution 45 mm -1
Day TV camera 117 x 53 x 91 mm Input faceplate Glass
Operation range (targetvehicle) 1.5 ÷ 2 km Output faceplate Fiber-optic plate
Spectral range 0.6 – 0.9 μm Screen Yellow-green
Effective scene illuminationRange
5x10-3 ÷ 5x104 lux Weight 150 g
Field of view: Dimension: ∅ 64 x 22 mm
Day: 13,5° x 18°
Night: 8,4° x 11° TV channel:Resolution: Sensor type: CCD matrix
Day: 500 TV lines Pixels number: 752 (H) x 582 (V)
Night:350-400 TV lines
Pixels size- anti blooming- gamma correction- electronic shutter
4,6 mm x 6,4 mm
Теchnical characteristics
GEO-NTK4I is used for recognitionthe away targets by the operator on the TV monitor thus the targets should be preliminary detected with a radar system. GEO-NTK4I is derived on base of Third Generation Image Intensifier Tube coupled with digital CCD camera. Third Generation image intensifier tube consists of: GaAs photocathode;
Micro channel Plate (MCP) and phosphor screen. GEO-NTK4I has the Day channel, which provides
automatic transfer from night to day regime by the video signal level control.
GEO-NTK4I has the special digital processor for image enhancement.
GEO-NTK4I is used for applying the unguided weapon at day & night time.
GEO-NTK4I based on the high technology.
GEO-NTK4I is used for acquiring and targeting short and intermediate range
targets.
GEO-NTK4I uses the TV monitor for detection & recognition targets.
GEO-NTK4I uses the digital processing the “night” imagery for increasing
detection range.
GEO-NTK4I has the low cost.
Active-pulsed Night Vision TVCamera GEO-NTK-4 I
Technical specification: System specification:
Operating range (people group) 1.5 ÷ 2 km Configuration Night TV camera
Spectral range 0.53 – 0.93 μm Television standard Day TV camera
Effective scene illumination range 5x10-4 ÷ 5x104 lux 625 lines, 25 hz
Field of view: TV dissector Horizontal, across-line
Day: 1.1° x 1.5° Power consumption 12 W, 0.5 A
Night: 2° x 3° Temperature of exploitation +40°C ÷ -40°C
Resolution: Weight TV camera 11 kg
Day: 570 TV lines Dimensions TV camera 350x310x230 mm
Night: 450 TV lines
Теchnical characteristics
Image intensifier tube III gen:
PhotocathodeType
GaAs Operating illumination Range
10-5 ÷ 10-1 lux
Photocathode sensitivity:
PhotocathodeDiameter
25 mm
Luminous 1800 μA/lm Resolution 36 lp/mm
Radiant 180 mA/W Output faceplate Fiber Optics
Signal/Noise 15 Input faceplate Glass
ratio (E=10-4 lux) Screen Yellow-green
Gain 35000
Background brightness
3x10-3
Laser channel specification:
Pulsed Laser Illuminator
L13
Field of view: 9° x 15°
Light wave 0,81 μm
Laser pulse length 120 HC
Delayed laser gate (0-15) μc
Gate pulse for IIT 5 μc
Pulsed radiated power 400 W
Frequency 5 kHz
Supply voltage: 12 V
Power consumption: 1.5 WSpecification TV channel:
Detector CCD matrix
Matrix size 4,6 x 6,8 mm
Pixels size 8,3 x 8,3 mcm
Pixels number- Protection againstthe optical jamming- Electronic shutter- Ggamma correction
752 x 582
GEO – NTK 4D is used for
recognition the away targets by
the operation on the TV
monitor.
GEO – NTK 4D is derived on
base CCD camera.
Augmented operating range at
the expense of usage IR spectral range
& digital processing imagery.
High technology recognition & low cost.
Augmented operating range at the expense of usage IR spectral
range & digital processing imagery.
Day TV Camera GEO-NTK4D
Specification technical:
Television standard 625 TV lines, 25 hz
TV dissector Horizontal, across-linePower consumption 12 W, 0.2 AOperating temperature range +55°C ÷ -50°C
Operating illumination range 0,1 ÷ 200 lux
Resolution 500 TV lines
Sensor type: CCD matrix
Pixel’s number: 752 (H) x 582 (V)
Pixel’s size 4,6 mm x 6,4 mmResolution > 500 TV linesDetektor CCD MatrixMatrix size 4,6 х 6,8 mmPixel’s size 8,3 х 8,3 mmPixel number 752 x 582Placement in consumer ingress protection
Equipment volume
Теchnical characteristics
GEO-PZR1 is intended for detection
and tracking the Air targets in
a night conditions on the upgraded
Complex. GEO-PZR1 is fixed on the
Air defence Complexes.
GEO-PZR1 has a special digital
processor for image enhancement.
High technology & low cost.
Fire by the defense complexes SA- 6
“KVADRAT”, SA-8 “OSA”, SA-11 “BUK”, SA-13
“STRELA-10”, SA-15 “TOR”
SA-19 “TUGUSKA” in a night conditions on heightened distances
in night conditions as possible.
Increasing detection distance by usage of IR spectral range & digital processing
of the “night” imagery.
Detection & recognition targets on the AMLCD..
Night TV-sighting system For Air defenseComplex GEO-PZR1
Technical specification: Image intensifier tube III generation:
Configuration Low-level TV camera
Photocathode GaSe
Television standart 625 lines, 50 Hz Photocathode sensitivity:
TV dissector Horizontal, across-line Luminous 1800 μA\Im (min)
Power supply 27 V, 0,5 A Radiant (λ=830nm) 180 mA\W (min)
Temperature of exploitation +50°С ÷ -40°C Gain 35000
Weight 15 kg Background brightness 6 x 10-3 (cd/m2)
Camera 400 x 270 x 120 mm Signal\noise ration (E=10-4) 15 (min)
Monitor 180 x 220 x 50 mm Working illumination range 10-5 ÷ 10-1 lux
TV channel: Photocathode diameter 25 mm
-Gamma correction: Yes Resolutions 32 lp\nm
-Electronic shutter: Yes Output window Twister 180°
- Antiblooming: Yes Input window Glass
Screen Yellow
Technical: TV channel:Operation range ( targethelicopterMil Mi-8)
10 km Sensor type CCD
Spectral range 0.58-0.93 nm Pixels number: 725 (H) x 582 (V)
illumination range 5x 10-3 ÷ 0.93 nm Working illumination rage 0.5 ÷ 150 lux
Field of view:
-Width 8° (H) x 6° (V)
-Narrow 24,7° (H) x 18.5° (V)
Resolution 350 ÷ 400 TV lines
Теchnical characteristics
GEO-PZR2 is intended for detection
and tracking the Air targets in a
night conditions on the AMLCD
for applying of Air Defence
guided missiles of the pgraded
Complex
GEO-PZR2 is fixed on the Air
defence Complexes.
Increasing detection distance by usage of IR
spectral range & digital processing of the “night” & imagery
High technology & low cost.
Detection & recognition targets on the AMLCD
Night TV-sighting systemFor Air defense Complex GEO-PZR2
Specification: Image intensifier tube III general data:
Television standart 625 lines, 50 Hz Photocathode GaAs
TV dissector Horizontal, across-line Photocathode sensitivity
Power supply 27 V, 0,6 A Luminous 1800 μA\lm (min)
Temperature of exploitation +50°C ÷ -40°C Radiant (λ=830 nm) 150 mA\W (min)
Weight 10 kg Gain 35000
Dimensions Background brightness 3x10-3 (cd/m2)
Camera 380 x 112.5 x 95 mm Signal\noise ratio (E=10-4 lux) 15
Monitor 294 x 245 x 92.5 mm Working illumination range 10-5 ÷ 10-1 lux
TV channel: Photocathode diameter 18mm
- Gamma correction: Yes- Electronic shutter: Yes- Antiblooming: Yes Resolution 36 lp\mm
Output window Fiber-optic plate
Input window Glass
Screen Yellow
Recognition range (at the natural nightillumination ~ 5•10-2 lx and normal weather) of the:
- men in the foliage: not less than 500 m
- cargo car: not less than 800 m
Теchnical characteristics
Third generation night sight “GEO
- ZRK 1” is designed for using with
Russian portable air defense
missile systems : “IGLA” ,
“STRELA”. The night sight
“GEO - ZRK 1” extends using
Russian portable air defense
missile systems up to level of starlight
overcast. Complex is capable to detect air
targets at ranges up to 8km. The night range of detection in
starlight condition is achieved by the expense of application in the
Night Sight “GEO-ZRK” highly sensitive and low noise 25 mm Gen (III
+ I) Image Intensifier Tube (IIT), which consists of IIT GEN III with
GaAs photocathode without Microchannel Plate (MCP), coupled
with IIT Gen I. The wide field of view of thr “GEO - ZRK 1” allows the
sight to be used for local surveillance.
The Night Sight “GEO - ZRK 1” adapter braket can be attached and
removed quickly.
Night Sight for portable Air Defense Complex GEO-ZRK1
General technical specification:
Spectral response 580 - 900 nm
Field of View 24°
Magnification 1,8
Resolution 2,1 cy/mr
Gain (adjusted) 1600…8000
Voltage 2,2-3,5 V
Battery live 8 hours
Power source 2V AA alkaline
Objectiv lens:
- Focal length 55 mm
Aperture 1:1,7
Eyepiece:
- Focal length 30,5 mm
Eye relief 25 mm
Output diameter 7 mm
Diopter adjustment +4…-6 dptr
Dimension 300 x 200 x 96 mm
Weight 1.6 kg
- with adapter 1.9 kg
Теchnical characteristics
GEO-KPP is intended for estimation
of light leakage to provide
adaptation of the aircraft
lighting compatible with
Aviator’s Night Vision Goggles
(NVG) on the basis of Third
Generation Image Intensifier
Tubes (IIT Gen. Ill)
Test Equipment for Estimation of theCompatibility Aircraft Interior Lighting with
Night Vision Goggles GEO-KPP
Technical specification:
Measuring spectral ranges forestimation of the adaptationquality:
350-930 nm
Measurement range of theradiant power ratio 0-100%
Accuracy: ± 0,05 %
Voltage 27 V
GEO-KPP weight: 3.0 kg
Теchnical characteristics
Visual supervision of objects at
night. Explaining on the ground
and water. Individual
adjustment under the
operator eyes. Border patrol
and security Ergonomic and
Esthetic Application of the
independent power supply
Pocketscope GEO M
System specification: Image intensifier tube Gen. III:Terrain illumination 5 x10-4 lux ÷ 0.1 lux Photocathode Type GaAs
Magnification 1* 2* 3* Photocathode Sensitivity
Field of View 40° 22,3° 13,6° Luminous 1500 μA/lm
Diopter adjustment +5,5 D -4,5 D Radiant (λ=830 nm) 150 mA/W
Voltage 3 V Gain 25000
Power supply 2 AA size Alkaline (316) Signal/Noise Ratio E=10-4 lux 20
Working time in normal climatic conditions
not less 10 h Center Resolution 45 mm-1
Useful Cathode Diameter 17,5 mm
Input faceplate Glass, С57
Output Faceplate Fiber Optics Inverter
Dimension ∅ 36,75 mm x 31 mm
Теchnical characteristics
Onboard weight-measuring system
(OWMS) is designed to measure
the load of heavy vehicles. In
case of exceeding the allowable
load it alarms. The information
about the vehicle is recorded on the
flash drive and could be transferred
to PC via USB or wireless.
OWMS provides information on
cargo weight and distribution of cargo weight on
the axes of the vehicle. These parameters are calculated from the data
obtained from sensors based on micromechanical accelerometers that are
part of OWMS.
The device displays also date, time and operating time of the vehicle in hours.
The device has built-in battery, rechargeable from the car power grid.
OWMS performs self-control of sensors serviceableness, communication lines
and in case of the presence of faults will display the diagnostic information on
the display.
The amount of memory provides the recording of the output parameters for
365 days.
On-board information measuring system
MAIN FEATURES:
Control and indication unit of the OWMS is made in a standard
head unit size as used for heavy-duty trucks manufactured by
“KAMAZ” group or any other (single DIN head unit);
error of weight measuring not more than 5% of the range of
measurement;
reading stored information under given protocol via USB or
wireless.
Micromechanical helmet–
mounted system of orientation
(HSO) is designed for
automatic definition of
angular coordinates
{ϕX; ϕY; ϕZ} of the boresight
line in the coordinate system of
the flying machine and transferring
these coordinates to the onboard complex of
radio-electronic equipment of the flying machine. The boresight line
is observed at a turn of a head and matching the target with the
image of shooting mark. MSISO for HMSTI at demonstration stand
1. Personal computer with “HSO” software;2. Autocollimating mirror;3. Reference node consisting of the attitude heading
reference system and autocollimating mirror;4. Optical Theodolite;5. Micromechanical helmet attitude heading reference
system.
Micromechanical helmet attitude heading reference system
Micromechanical Helmet-mounted system of orientationfor system of targeting and indication
Specifications of HSO:
Range of measurement the angularcoordinates of the boresight line
Azimuth:Elevation:Roll:
ϕY= ± 110° ϕZ= ± 80° ϕX= ± 60°
The accuracy of measurementthe angular coordinates of theboresight line
Δ ϕY = 3,0°Δ ϕZ = 1,5°Δ ϕX = 1,5°
Теchnical characteristics
Tiltmeters based on
MEMS - accelerometers
are designed measuring of the
tilt angle of any objects or
surface relief relative to
the lo cal horizon. Features:
small dimensions, weight
and power consumption.
Fields of application:Motor vehicle and civil engineering:
traffic safety systems;sensors for controlling threshold value of angle;
Oil and Gas Industry and robotic complexes:control of drilling tools, pipelines and processing equipment;on-line monitoring of buildings and environment;
Medicine:tilt angle sensors for medical beds, tables and invalid chairs;medical robotics complexes.
Aviation Industry:Electronic quadrant for mounting of helicopter equipment.
Tiltmeters based on mems-accelerometers
APPLICATIONS
PARAMETERS
Automobile transport
and constructionmachinery
Medicine Military roboticComplexes
Aviation Industry
LinearaccelerationRange
± 10 g ± 2 g ± 1,7 g ± 1,7 g
Accuracy of linearaccelerationMeasurement
0,5% 0,5% 0,1% -
Two-Axes anglesmeasurementRange
± 70° ± 90° ± 60° ± 45°
Angular positionmeasurementError
0,3° 0,5° 0,1° 0,05°
Dimensions ∅ 49 x 25 mm ∅ 32 x 25 mm ∅ 32 x 25 mm 140 x 140 x 60 mm
Voltage Supply (V) 12 V 12 V 12 V 12 V
TemperatureRange -40 + 85°C -10 + 70°C -40 + 85°C 16 ÷ 35°C
Interface CAN/RS232 RS232 RS232 RS232
Теchnical characteristics
Measuring the distance to theobject, its geographical coordinates within a few seconds accuracy; - Displaying parameters (date, time, distance and geographical coordinates) of the object of observation in real time in the cam-
era viewfinder or on the camera LCD; - Full HD video recording
(1920x1080px) and pictures of the remote object with superimposed coordinate information
at the bottom of the frame;
Small dimensions and weight of the device;Hand held or tripod mount.
1. Model of the device with a camera2. Prototype of the device with a video camera and a tabletPC
Fields of application:protection of state and administrative boundaries;patrolling of the territory;
Observing device for determining the geographicalcoordinates of remote object With the micromechanical
strapdown inertial navigation system
08.12.2009 / Distance: 350 m Object: Lon.: 37,2347Lat .:55,4567 H. 124 10:45:78Azimith: 12 Observer: Lon.: 37,2447 Lat .:55,4667 H. 156
General description:
Composition DSLR camera, laser range finder, GPS/Glonass receiver, strapdown integratednaviga- tion system MEMS-based, module ofinformation pro- cessing, microdisplay withcollimating optics
Time of measurement 0,3 s
Mass 3 kg
Operating temperature 0 ÷ 40 °C
Range of distance measurement +5 ÷ 40 °C
The accuracy of determininggeographi- cal coordinates of the
remote object
± 2” for latitude and longitude,±100 m for height
Overall dimensions 280 x 230 x 175 mm
Technical data:
Type of laser Class 1, eye safe,λ=905 nm
The accuracy of determining the distance ±1m
Video frame rate 30, 25, 20 Hz
Video frame size 1920 x 1080
image size 3872 x 2592
The accuracy of the observer’s coordinatesDetection
11 m
The range of measured azimuth 0–360є
The accuracy of azimuth defenition* ± 2°
The measurement range of pitch and rollAngles
± 70°
Теchnical characteristics
* Is reached under the pre-calibration and the absence of external magnetic fields in thearea of measurement.