Male UCAV



The SHAHPAR-III is a Medium Altitude Long Endurance (MALE) Unmanned Combat Aerial Vehicle (UCAV) designed to deliver superior performance in surveillance, reconnaissance, and combat missions. Shahpar-III is a testament to GIDS' commitment to innovation and excellence in defense technology. Its combination of advanced features, robust design, and versatile capabilities make it an indispensable force multiplier for modern military operations

SPECIFICATIONS
Data Link Range 250 + km (LOS)
2500 + km (BLOS)
5000 km with SATCOM
Endurance 30 Hrs (ISR)
16 Hrs (Armed)
Altitude Ceiling (Max) 30000+ Ft (ISR)
28000+ Ft (Armed)
Wing Span 65ft
Internal Payload 125 kg (ISR)
75 kg (Armed)
External Payload 570 Kg (06 x Hard points)
Max Take-off Weight 1600 kg
Engine 140 HP

FEATURES
  • Armed capability (06 wing hard points)
  • Molded High Strength Composite Structure
  • Retractable landing gears
  • Satellite Link (SATCOM)
  • ATC Transponder / IFF
  • Indigenously developed Avionics Systems
  • Dual redundant Flight Control Computer, Power Management System, Engine Control Computer, Payload Management Computer, Data Links, Control Servos
  • Multiple Payload Carriage: EO / IR, SAR, COMINT / ELINT
  • Image based accurate Geo Referencing
  • Live and post flight video processing for AI based target detection and identification
  • Group 4+ category UAV

UCAV System



SHAHPAR-II Block-ll is a medium-altitude, long-endurance unmanned aircraft with armed capability. It has a modular airframe structural design comprising of advanced composite and metallic hybrid structure. Salient features include autonomous take-off and landing, robust autopilot scheme, user-friendly and comprehensive mission planning & management software suite in Ground Control Station, multiple redundant data links, and capability of integrating various types of payloads and weapons.

SPECIFICATIONS
Data Link Range 250 km (LOS ) 1500 km (BLOS)
Endurance 20 Hrs (ISR) 15 Hrs (Armed - 60kg External Payload) 12 Hrs (Armed - 120kg External Payload)
Altitude Ceiling (Max) 25,000 Ft (ISR) & 22,000 Ft (Armed)
Wingspan 35 Ft
Internal Payload 75 kg
External Payload 120 kg (04 x wing hard points)
MTOW 1125 kg
Engine 140 HP Turbo-charged Engine with Intercooler

Features
  • Optimized Aerodynamics & Structural Design
  • Dual redundant Avionics Suit and Navigation systems
  • Triple redundant Communication Data Links
  • Optional Payloads (COMINT / ELINT, SAR, HD EO / IR)
  • Satellite Link (SATCOM)
  • ATC Transponder
  • VHF-RT voice relay
  • Internal Pilot Option
  • Retractable Landing Gears
  • Asymmetric Landing and Takeoff
  • Mid-air Engine Restart Capability
  • Low acoustic signature
  • Laser guided missiles with CEP less than 1.5 m
  • Integration of 3rd party payloads and weapons
  • User friendly Ground Control Station (GCS) with 02 UAVs operations simultaneously
  • Advanced Ground Data Terminals (GDTs)
  • Advance Simulators for pilot training
  • Advance O & I level test equipment
  • Effective Life Cycle Support with comprehensive Spares Package

TACTICAL UAV SYSTEM

Uqab NG meets the challenging demands of Intelligence, Surveillance & Reconnaissance (ISR) in the battlefield. With a Range of 150 km, Endurance of more than 8 hours & Flight Ceiling of 18,000 ft, Uqab NG offers all operational features of a state of art Tactical UAV System. It has effectively been used in Counter Terrorism Operations in Pakistan. Uqab NG is a battle hardened UAV with built in redundant systems & fail safe features. It has been designed & manufactured to meet stringent Military & Aviation standards. With the capacity to carry more than 15 kg payload, modern Digital Tactical Data Links, user friendly multi UAV operation capability & proven robustness & reliability, Uqab NG offers features comparable to any modern UAS.


Specification
Range 150 km LOS
Endurance 8 Hrs
Service Ceiling 5,500m (18,000 ft) AMSL
Takeoff Weight 100 ± 10 kg
Payload < 15kg
Gyro stabilized, Multi Senor POD with Full HD Day & Night (TI) video & AI features
Navigation RTK based Tri Constellation DGNSS, Magnetic Compass based Dead Reckoning
Communication System C-Band, encrypted, HD video
Launch / Recovery Hydro-pneumatic Launch / Hoisted Net System & Emergency Parachute
GCS Environmentally controlled cabin with stand alone consoles

Features
  • FAR-23 compliant airframe
  • Low SWAP MIL STD home grown Flight Controller & GNC System
  • Inbuilt redundancies & automatic fail safe / emergency procedures
  • HD video with Cooled Thermal Imager with AI based tools
  • EFI based High Efficiency Engine
  • Catapult Launch & Net Landing with Parachute Emergency Recovery
  • Hybrid Electric Vertical Take off & Landing Version (under development)

Mortar Carrier Hexacopter

Beetle is a versatile and robust Mortar Carrier Hexacopter for modern military and tactical operations, engineered for Intelligence, Surveillance, and Reconnaissance (ISR) missions, as well as the precise engagement and neutralization of targets. This advanced hexacopter is designed to meet the rigorous demands of modern tactical operations.


FEATURES
  • Multiple Mortar Payloads Dropping Capability
  • Day/Night Intelligence, Surveillance & Reconnaissance Missions
  • Complete Autonomous Operation with pilot override option
  • Modular, man-portable
  • Handheld GCS consoles for AV & payload operator
  • Fast redeployment / turnover

SPECIFICATIONS
Airframe Hexacopter configuration, carbon fiber structure, man portabal
Camera Day: 40x Optical Zoom, 1080p, 30fps
Night: 640 x 512, 25 Hz, TI Lens (50 mm)
Payload Capability 3 x 60 mm Mortars
Hit Accuracy (at 500m) 10 m
Endurance 60 mins in ISR Mode
40 mins with Max Payload
MTOW 28 kg
Range 5 ~ 7 km
Max Service Ceiling 3500 m AMSL
Wind Resistance 14 m/s
Dimensions 1650 x 1650 x 750 mm
Navigation Multi GNSS (GPS + GLONASS + BeiDou + Galileo)
Telemetry Flt Modes, Voltage indicator, Signal strength, Flt Altitude / Attitude / Distance & Speed
Failsafe Auto Return to Base / land in case of low battery & link failure

Mortar Carrier Quadcopter

Beetle is a versatile and robust Mortar Carrier Quadcopter designed for modern military and tactical operations, ensuring mission success through advanced technology and innovative design. Beetle is designed for Intelligence, Surveillance, and Reconnaissance (ISR) missions, as well as precise engagement and neutralization of targets. This state-of-the-art quadcopter offers unparalleled capabilities for modern tactical operations.


FEATURES
  • Multiple Mortar Payloads Dropping Capability
  • Day/Night Intelligence, Surveillance & Reconnaissance Missions
  • Complete Autonomous Operation with pilot override option
  • Modular, man-portable
  • Handheld GCS consoles for AV & payload operator
  • Fast redeployment / turnover

SPECIFICATIONS
Airframe Quadrotor configuration, carbon fiber structure, man portable
Camera Day: 40x Optical Zoom, 1080p, 30fps
Night: 640 x 512, 25 Hz, TI Lens (50 mm)
Payload Capability 2 x 60 mm Mortar
Hit Accuracy (at 500m) 10 m
Endurance 60 mins in ISR Mode
40 mins with Max Payload
MTOW 18 kg
Range 5 ~ 7 km
Wind Resistance 14 m/s
Dimensions 1230 x 1230 x 690 mm
Navigation Multi GNSS (GPS + GLONASS + BeiDou + Galileo)
Telemetry Flt Modes, Voltage indicator, Signal strength, Flt Altitude / Attitude / Distance & Speed
Fail-safe Auto Return to Base / land in case of low battery & link failure

Surveillance UAV

Ranger is a Hybrid VTOL Surveillance UAV offering runway independence, unprecedented endurance, innovative modularity and rapid emplacement. It is designed for expeditionary Land and Sea operations with a useable payload capacity of up to 5-10 kg. Ranger offers flexible payload options utilizing industry leading imaging sensors such as long range EO / MWIR as well as on board tracking, stabilization and video processing. Expanded size, weight and power (SWAP) profile makes Ranger an ideal choice for Intelligence, Surveillance, Target Acquisition, Reconnaissance (ISTAR) and Artillery Fire Correction (AFC) roles.


FEATURES
  • Vertical Take-off and Landing
  • Reduced operational footprint and transportation loadout
  • Covert missions with negligible visual and acoustic signature
  • Autonomous missions
  • AI cameras with auto detection and tracking
  • Digital datalink
  • Fault-tolerant flight control system with redundant IMUs
  • Auto return to base / land in case of low battery & link failure
  • Open system architecture for customer-defined payloads From transport to flight in less than 30 minutes with 4
  • men crew
  • Small portable ground station

SPECIFICATIONS
MTOW 65 ~ 70 kg
Wingspan 4.8 m
Length 2.58 m
Endurance 6 ~ 8 hrs
Control Radius 100-150 km
Maximum Altitude 4500 m AMSL
Wind Resistance Level 7 (28~37 Knots)
Operational Temperature -10~ + 55°C
Powerplant 2-Stroke EFI Engine
EO / IR Payloadn EO: 30X Optical Zoom, 1080p FHD
Cooled IR: 640 x 512 with 5-10X Optical Zoom
LRF: 8 - 12 km
Artillery Fire Correction Accuracy 10-15 m using AI based Geo Ref Algorithm

Surveillance UAV

Scout is designed for Intelligence, Surveillance, Target Acquisition, Reconnaissance (ISTAR) and Artillery Fire Correction (AFC) roles. For its small size, Scout offers exceptional performance. Scout carries a multi-sensor gimbal payload, capable of detecting, recognizing and identifying enemy targets during day and night missions while flying at altitudes up to 1500 m Above Ground Level (AGL). With an operating radius of up to 50 km and a service ceiling of 4500 m Above Mean Sea Level (AMSL), it is a potent tool for militaries and paramilitaries.


FEATURES
  • Vertical Take-off and Landing
  • 3.5 hours endurance
  • Exceptional flight time in its weight class
  • Fully Autonomous Missions
  • AI cameras with Auto detection and tracking
  • HD Digital Datalink
  • Fault tolerant flight control system with redundant IMUs
  • Auto Return to Base / Land in case of low battery & link failure
  • Battery powered all electric propulsion
  • Low acoustic and visual signature
  • Complete sys assembly in 15min with 2-3 men crew
  • Small Portable Ground Station

SPECIFICATIONS
MTOW 17 kg
Wingspan 3 m
Length 1.8 m
Endurance Up to 3.5 hrs
Control Radius 50 km with Ground Antenna Tracker
Cruise Speed 65~80 km/hr
Cruise Altitude 1000~1500 m AGL
Wind Resistance Level 6 (22~27 Knots)
EO / IR Payload EO: 30X Optical Zoom, 1080p FHD
(Gyro Stabilized) IR: 640x512, 50mm lens, 12µm pixel pitch
LRF: Up to 2.5 km
Navigation Multi GNSS (GPS + GLONASS + BeiDou + Galileo)
Artillery Fire Correction Accuracy 10-15 m using AI based Geo Ref Algorithm



General purpose bombs are effective against all kind of targets. The bombs give blast as well as fragmentation effect. Low-Drag design with high Length-to-Diameter Ratio. Forged from seamless steel tube. Filled with Compo 'B' explosive. Inert illing can be used for training purpose.

  • PK-81 (120 kg)
  • PK-82 (250 kg)
  • PK-83 (500 kg)
  • PK-84 (1000 kg)
  • Can be used in the following configurations
  • Low drag configuration: when installed with Conical Fin Assembly
  • High drag configuration: when installed with Retarded Tail Unit
  • Can be itted with the following types of fuzes
  • Mechanical Nose fuze M-904 or equivalent
  • Mechanical Tail fuze M-905 or equivalent
  • FEATURES
  • Can be carried on NATO standard suspension systems
  • Can be itted with the following types of Electronic fuzes
  • Ultra Quick Electronic Impact Nose Fuzes AB-100( in low drag configuration) and AB-105(in low or high drag configuration)
  • Electronic Proximity Nose Fuzes AB-103 (in low drag configuration) and AB-104 (in low or high dragconfiguration)
  • Electronic Long Delay Fuze AB-112 Electrically Timed Fuzes FMU-81/B, FMU-139 A/B

Pre-Fragmented bombs are based on new concept in optimizing the effectiveness of conventional munition. Outer casing is manufactured from composite iber. Bomb contains spherical steel balls which shoot out in all directions when the blast occurs. Extremely effective against soft targets at longer distances from the point of detonation 5 to 6 times more effective than a General Purpose Steel Bomb. High Length-to- Diameter Ratio for low drag design. Can be used in the following configuration:

  • Low drag configuration: With Conical Fin Assembly
  • High drag configuration: Installed Retarded Tail Unit


Features
    NATO APPLICATIONS:
  • It can be carried on NATO standard suspension system.
  • It can be fitted with the following types of fuzes:-
    • Ultra Quick Electronic Impact Nose Fuzes AB-100 (in low drag configuration ) and AB-105 (in low or high drag configuration)
    • Electronic Proximity Nose Fuze AB-103 (in low drag configuration) and AB-104 (in low or high drag configuration).
  • WARSAW APPLICATIONS:
  • Includes Integral E.F.I Cable for interfacing the nose fuze to Russian aircraft pylons.
  • Can be carried on WARSAW standard suspension systems.

THERMOBARIC BOMBS

GIDS specializes in the production of thermobaric general-purpose bombs which are characterized by large blast and high thermal energy. These explosives are particularly effective against tunnels, bunkers, shelters, buildings and caves etc.


SCP-5 is a hard nose penetrator that is housed within Mk-82 Form Factor. It is highly effective against hardened bunkers, bridge, piers and A/C pens. The penetration is maximized through kinetic energy gained by bomb as it follows its ballistics. The bomb has a dynamically stable explosive specifically required for penetrators.


Features
  • Penetrates four double-reinforced concrete walls / floors 200mm thick each
  • Penetrates 1.5m in 35MPa reinforced concrete target
  • Can be used as an effective stand off weapon in combination with a Range Extension Kit
  • Compatible with all guidance systems
  • Qualified to MIL STD 810H

Main Specifications
Penetration in 5000psi reinforced concrete target 1 ~ 1.5 meter
Max Fragment Lethal Range > 250m
Explosive Dynamic Shock Capacity Mach 3 Impact
Max Blast Over Pressure (open envirnment) 17.5 g/cm3

ZUMR – IlI is a high-performance, high-definition Multispectral Imaging (Vis/NIR, SWIR, MWIR) payload with 24/7 mission capability with enhanced image stabilization. It supports INS, GMTI, and Geo-Referencing, ensuring 24/7 mission capability for SHAHPAR III and other platforms, enabling precise munitions delivery, battlefield damage assessment, and search and rescue operations.

FEATURES

High performance High Definition Multispectral Imaging System
24 / 7 Mission Capability with Enhanced Imagers
Highly Stabilized System
Single LRU based Designation System

MISSIONS

High Definition Aerial imagery
High performance EO / IR payload for precision munitions (LGB, Missile) delivery
Battlefield Damage Assessment
Search and Rescue
Tactical Support

TECHNICAL CHARACTERISTICS

4 axis gyro stabilized system
Azimuth 360° continuous
Elevation +90° to - 110°
Weight>75 Kg

SENSOR CONFIGURATION
Thermal Imager
Resolution 1280 × 1024
Field of View:
-Wide 30° × 24°
-Medium-Wide 7.89° × 6.3°
-Narrow 0.97° × 0.76°
-Super-Narrow 0.72° × 0.57°
Short Wave IR
Resolution 1280 × 1024
Field of View: 0.5° × 0.40°
Day Imager
Resolution 1920 × 1080
Field of View: 24° - 0.70°
Laser Designator
Range 20Km
Energy 85 mJ / 160 mJ
Wavelength 1064nm
Code NATO, Custom
Laser Range Finder
Range >32Km
Wave Length 1540nm

DAY / NIGHT SURVEILLANCE & TARGETING PAYLOAD

ZUMR - Il (HD) is a high definition, high-performance Multispectral Imaging payload with 24/7 mission capability with enhanced imagers. It is highly stabilized system with 2 LRUs (Line Replaceable Units). The multi-sensor Optronic Payloads can provide geo-referenced Day, Near Infrared and Infrared imagery to battlefield commanders for reconnaissance and designation purposes. The Electro-Optical Payloads can be integrated on Fixed-Wing manned and unmanned aerial platforms as well as on Helicopters.

FEATURES

High performance HD Imaging
24/7 Mission Capability with Enhanced Imagers
Highly Stabilized Turret
Superior Image quality
2 LRUs (Line Replaceable Units)

MISSIONS

High Definition Aerial Imagery
High performance EO / IR payload for precision munitions (LGB, Missile) delivery Battlefield Damage Assessment
Search and Rescue
Tactical Support

TECHNICAL CHARACTERISTICS

4 axis gyro stabilized system
Azimuth 360° continuous
Elevation -20° to +100°
Weight 50 Kg

OPTIONS

System Coupling: GPS, INS, Radar, Moving Map Interactive
Customized GUI to reduce operator fatigue, Image Enhancement
Geo-Pointing, Geo-Referencing, Geo-Lock Modes

SENSOR CONFIGURATION
PLATFORMS UAVS, Aircrafts, Helicopters, Naval Ships
Thermal Imager
Resolution 1280 × 1024
Field of View:
-Wide 30.25°H × 17.4°V
-Medium-Wide 4.85°H × 2.71°V
-Narrow 1.52°H × 0.87°V
-Super-Narrow 0.76°H × 0.43°V
(2x E-Zoom)
Laser Rg Finder
Range 20 Km
Wave Length 830
Laser Designator
Range > 30Km
Energy 85 mJ / 110 J
Wavelength 1064nm
Code NATO, Custom
Enhanced Day Imager
Resolution 1920 × 1080
Field of View 36.6° - 1.52°

LIGHT WEIGHT HD SURVEILLANCE PAYLOAD

NAHL is a Light weight HD Surveillance Payload with Single LRU based surveillance system and highly stabilized Multispectral Imaging. It has 24/7 mission capability with enhanced imagers; Day and Night surveillance of site (offshore platforms, industrial and sensitive sites), border surveillance & homeland security.


FEATURES
  • Light weight suitable for small UAVs,
  • Single LRU based surveillance system
  • Highly stabilized Multispectral Imaging
  • 24/7 Mission Capability with Enhanced Imagers
  • Day and Night surveillance of site (offshore platforms, industrial and sensitive sites) Border surveillance, Homeland security tracking and Tactical support

SENSOR CONFIGURATION

PLATFORMS
UAVS, Aircrafts, Helicopters, Naval Ships
Aerostats and Ground Based Vehicles for area monitoring


Thermal Imager SD
Sensor 640 x 512 MCT
Field of View:
Wide 16°H x 12°V
Narrow 1.8°H x 1.35°V
Zoom 9x (Optical)
Day Camera HD
Resolution 1920 x 1080
Field of View:
Wide 63.7°H x 47.7°V
Narrow 2.3° H x 1.7°V
Zoom 30x (Optical)

Spotter Scope/NIR HD
Resolution 1920 x 1080
Field of View:
Wide 24° H x 13°V
Narrow 0.9° H x 0.5°V
Zoom 27x (Optical)
Laser Range Finder & Laser Pointer
Range 15 Km max
LP NVG Compatible (150 mW)

COMINT Payload is meant for high performance Interception and Direction Finding, Multi channels Monitoring on the move, Target Geo Location and real time Automatic Modulation Classification of standard civil and military signals.


SPECIFICATIONS
Frequency Range 30-6000 MHz
Direction Finding Localization and Analysis with DF accuracy up to 20 RMS
Detected Hop features Hopping frequency-list, Hop Rate , Dwell Time , Hopping Amplitude
Features Hop Rate : 1000 Hops/s
Spectrum Monitoring and Analysis Modulation Detection :
Complete Analog & Digital (Basic to Higher Orders) Modulation
Voice extraction for analog radios
Voice/ data for digital radios (Non encrypted & standard signals)
SWAP
Size LRU 1 : 387 x 283 x 65 mm
LRU 2 : 350 x 278 x 79 mm
Weight 20 Kg
Power 250 W at 28 VDC

ELINT system is designed for the dense and most complex electromagnetic environments meeting the rapidly evolving needs of today's modern battlefields. The system delivers sophisticated intelligence gathering capabilities for the detection and analysis of all types of radars including LPI, Fire Control, Surveillance and Tracking, Navigational Radars for Ground based, airborne and shipborne applications. Based on the advanced hybrid architecture, ELINT simultaneously detects and identifies multiple radars, fine direction and target geo-location. It acquires radar signals at a very high level of accuracy and clearly distinguishes between them by rapidly measuring and processes the data. It is capable to graphically display the Electronic Order of Battle for the operator in real-time. The system can be integrated with stand-off jamming as a part of airborne EW suite


FEATURES
  • High Probability of Intercept (POI)
  • Wide Frequency and DF coverage
  • High DF and Frequency accuracies
  • High system Sensitivity and Dynamic Range
  • Multiple Instantaneous Bandwidths (Both Wide and Narrow bands)
  • Capable to handle complex and dense EM environment with high parameter extraction accuracies
  • Geo-location and Data Recording Capability
  • Mission Specific Threat Library
  • Low SWAP Modular architecture
SPECIFICATIONS
Weight Approx 30 kg
Freq coverage 2-18 GHz (0.5-2 GHz optional)
Sensitivity Better than -80 dBm
Dynamic Range 70 dB
DF Accuracy: Better than 2 deg RMS
Power Req 380 W
Sizes (H x D x W) mm 130 x 98 x 275 (ADF Unit)
155 x 59 x 616 (Pl unit)
271 x 248 x 210 (RPU)

BURQ

BURQ-50P having enhanced lethality is a state-of-the-art laser guided propelled weapon with high precision and hit accuracy. It has capability to hit static and moving targets. Different types of WHs can be integrated with this weapon as per target type and operational requirement. It can be mounted and fired from UAVs as well as from combat Helicopters. Laser designation can be done from on-board EO-payload or ground designator. It can support both lock-on before launch (LOBL) and lock-on after launch (LOAL) modes of operation. BURQ 45P is a state-of-the-art laser guided propelled weapon with high precision and hit accuracy. It is capable to hit static and moving targets. Different types of warheads can be integrated with this weapon as per target type and operational requirements, It can be fired from combat Helicopters and UAVs. Laser designation can be employed through on-board EO payloads as well as ground designators, It can support both lock-on before launch (LOBL) and lock-on after launch (LOAL) modes of operation: BURQ 25G is a state-of-the-art laser guided glide weapon with high precision and hit accuracy. It can be launched from smaller UAVs with lower payload capacity. It has capability to hit static and moving targets, Laser designation can be done from on-board EO-payload or ground designator. It can support both lock-on before launch (LOBL) and lock-on after launch (LOAL) modes of operation.


Performance Characteristics

Parameter BURQ (50P) BURQ (45P) BURQ (25G)
Range 2.5 - 12.0 km 2.5 - 12.0 km 3.0 - 12.0 km
Diameter 180 mm 180 mm 160 mm
Wing Span 380 mm 380 mm 480 mm
Length 1450 mm 1450 mm 1000 mm
Weight ≤ 50 kg ≤ 45 kg ≤ 25 kg
Warhead Mass ~ 20 kg ~ 10 kg ~ 9 kg
Warhead Type Blast Fragmentation
Penetration WH
Anti-Armor
Blast Fragmentation
Penetration WH
Shape Charge
Blast
Fragmentation
Warhead Fuse Type Electro-mechanical Electro-mechanica Electro-mechanica
Guidance System Semi-active Lase
Homing Guidance + GNSS (Optional)
Semi-active Laser
Homing Guidance
Semi-active Laser
Homing Guidance + GNSS (Optional)

AL BATTAAR

Al Battaar is a laser guidance bomb kit attached to the nose and tail of the GP (General Purpose) Bombs. It can be carried and launched from all NATO aircraft and is designed for use when attacking soft, hard, slow moving and stationary targets. The weapon will operate from a variety of different launch scenarios (high/ low altitude, level/ dive/ loft deliveries).
Al Battaar is capable of a single or multiple carriage on host aircraft. Guidance is provided by laser energy reflected from the target. Target illumination, may be provided by the delivery aircraft, another aircraft, or a ground designator. Flight can be divided into three phases: Ballistic, Acquisition, and Terminal Guidance.


Performance Characteristics

Feature Specification
Impact Accuracy / CEP <= 10 meter
Max Release Altitude 25000ft
Range 8 nm
Guidance Laser
Employment Mode Single
Laser Designated Compatibility Yes
LSHA FOV ±12deg
Field of Regard ±18deg
Laser Code Yes
Missing Pulse Logic Yes
Field Replaceable Electronic Tray Yes
Carriage Vibration 6.3g
Carriage speed limit 1.4M
Carriage Vibration 6.3g
Release speed limit 1.2M
Acquisition Range (NOMINAL) 12000ft
Canard Travel ±10.5deg
Laser Coding PRF Selection Enabled
Maneuverability (500 KTAS, SL) 2.8g

TAKBIR

REK converts the General Purpose Steel Bombs to guided weapons by simply integrating the Range Extension Kit. The kit includes a Tail Unit integrated with the bomb body that provides both guidance and navigation to the target, and an additional Wing Unit (with deployable wings) for extending the range.


Characteristics Specifications
Range 100 km
Launch Speed 0.6 - 0.8 Mach
Launch Altitude ≤ 9000 m
Weight with 250Kg GP Bomb < 300 kg
Interface RS 422 / Mil-Std-1760
Accuracy (with GPS) < 10 m CEP
Flight Time ~5min

Main Features
  • Autonomous guidance by means of an onboard AHRS
    System aided by a Global Positioning System (GPS) processor.
  • All Weather Weapon.
  • Capable to accept precise targeting information in the form of World Geodetic Survey (WGS)-84 coordinates provided either during mission planning or in flight.
  • Environmental Test Methods as per MIL STD 810F.
  • Specification Practices as per MIL STD 490A.
  • Defense System Software Development as per MIL STD 498.
  • Control of EMI as per MILSTD 461D.

SSMDR

SSMDR is designed to capture high resolution synchronized videos using state of the art CCD camera technology and high speed data recording on solid state media.


DVR Main Features
  • Simultaneous 2 Video / Audio Channel Recording
  • Continuous Recording upto 3 hrs
  • HUD, REO or MFD Recording
  • Records in standard MPEG-4 format
  • Supports, NTSC, PAL, composite
  • GPS time tagging for synchronized playback
  • Trigger event / Event Mark recording, video overlay and audio tone
  • Solid State Compact Flash Recording media (current 16 GB, extendable with no hardware / software mod)
  • Qualified as per Mil-Std-810E, Mil-Std-461D/E,
  • Mil-Std-704

Infrared Flares (CMF-1, CMF-2, CMF-3)

IR-Flare provides an aircraft airborne countermeasure capability to dispense flare pellets to prevent interception by heat-seeking missiles. Upon actuation electricity, it ejects and ignites a pellet which produces infrared radiation according to black body radiation phenomenon.


CMF 1 CMF 2
Aircraft NATO Chinese
Dispensers ALE 29A,ALE39,ALE 47 GT-1,GT-1P
Firing Requirement O5A pulse for 50 ms 0.7 A pulse for 35 ms
Burning Time > 4 Sec >4 Sec

Chaff & Flare Dispenser System (MOHAFIZ)
  • Chaff & Flare dispenser system(Mohafiz) is an electromagnetic (RF) and Infrared (IR) countermeasure
    self-protection dispensing system for airborne objects
  • Chaff gives protection against Radar Guided Missile and Flare protects against infrared guided missiles
  • When this system is integrated with radar warning receiver (RWR) and missile approach warning system
    (MAWS), the Mohafiz CFD system is effective in multiple threat environments.

OVERVIEW

Mohafiz Chaff & Flare Dispenser System is an Electromagnetic (RF) and Infrared (IR) countermeasure self-protection dispensing system for airborne objects. Chaff gives protection against Radar Guided missile, whereas, Flare protects against Infrared Guided missile. The system can be operated in four different modes:-Trigger, Semi Auto (manual), Auto (Integrated with RWR) and Emergency.
The system qualifies following requisite Standards:-

  • MIL-STD-704A
  • MIL-STD-810E
  • MIL-STD-461D
  • DO-178
  • Power
  • Temperature & Vibration
  • EMC & EMI
  • Software

FEATURES
  • System Power Requirements - 28V DC @ 1 Amps
  • Coupled with Weight-Off-Wheels (WOW)
  • DCU (for controlling the modes of CFD and presentation of Chaff and Flare load count
  • Dispense Buttons - for dispense command
  • Power up Built in Test (BIT)
  • Automatic detection of Chaff/Flare magazines
  • Displays inventory of Chaff & Flare Cartridges
  • Automatic misfire detection, correction and compensation
  • Capable to dispense Chaff, Flare or both or Pre-programmed sequence of Chaff/Flare
  • Flexible to adopt Fighters & Transport aircraft, Helicopters
  • Interface available for RWR and MAWS
  • Manual Modes (0 to 9) are Flight-line programmable
  • Chinese and Pakistani origin Chaff & Flare cartridges can be used

OVERVIEW

The ACMI System is a cost effective training aid for combat mission. It employs advanced technologies to offer realistic recreations of combat missions. The airborne components of the system tap the data from the avionics bus of the aircraft thus offering very accurate and realistic recreations of air combat missions.

The system can be used both in Ranged as well as Range-less configurations. All the hardware and software technologies used in the development of the system are commercially available thus minimizing product support risks


FEATURES
  • Comprehensive Post-mission Debriefing withsynchronized AVTR display
  • Advanced 3D graphics for realistic recreations of missions
  • Real-time recreation of mission
  • Real-time data link for inter-aircraft and ground data communication
  • Safety and training related warnings
  • Acquisition of aircraft data using the MIL-STD-1553 and RS-232 avionics buses
  • Ground-based Debriefing stations can be used in standalone as well as networked environment
  • Tools for easy sharing of ACMI missions among various squadrons

OVERVIEW

Pylon-325/327 is designed for installation under the centerline (Fuselage) station of all Mirage aircraft to carry and release stores up to 1400 kg.


FEATURES

PHYSICAL CHARACTERISTICS

  • Main Components
    Length 3060
    Width 310
    Height 120
    Weight (kg) 92±4
  • Ejector Release Unit Type 115A Including I-28 Cartridges

TECHNICAL CHARACTERISTICS

Main Components
Attachment Under centre line station of Mirage aircraft with two ball suspension devices (Bush Assy)
Carrying System
  • Two hooks 30" apart. Maximum Load 1400kg
  • Two hooks 14" apart, Maximum Load 630kg
Release System Two Electrically fired I- 28 Impulse cartridge
Ejection Piston Stroke 2 38.5mm
Explosive Device Selection Fuze Arming Unit with Limped Loop ejection
Ejection Speed 6 to 7 m/sec with I-28 Initiator with weight of 2 50kg
Pylon Electrical Supply 24-28 VDC
Consumption per release sequence 3A per Impulse cartridge for less than 20ms
Consumption of each Fuze arming unit 0.2 to 0.4 A