Pr 1 00002

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



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


20 Eye relief 23 mm

Center Resolution 50 mm-1 System distortion Less than 2 %


17,5 mm Resolution 0,65 cy/mrad

Input faceplate Glass, C57 Focal length 25 mm


F Number 1,2


Input voltage 27 volts DC

Input currant 50 mA


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


54 ÷ 72 mm

Diopter +2D to -4D


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



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


17 Eye relief 23 mm

Center Resolution 36 mm-1 System distortion Less than 2 %


17,5 mm Resolution 0,65 cy/mrad

Input faceplate Glass, C57 Focal length 25 mm


F Number 1,2


Input voltage 27 volts DC

Input currant 50 mA


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


52 ÷ 72 mm

Diopter +2D to -4D



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


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


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


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


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


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


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


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


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


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


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


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


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


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


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


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


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


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




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°


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


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 processing, 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°


* Is reached under the pre-calibration and the absence of external magnetic fields in thearea of measurement.

Date post:	23-Jun-2015
Category:	Technology
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