UAV System



Shahpar-II Block II 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 with improved aerodynamic design. Some of the notable features of the Shahpar system include its autonomous take-off and landing system, a robust autopilot scheme, user friendly and a comprehensive mission planning and management software suite, reliable data links and the capability of integrating various types of EO payloads.

Performance Characteristics
Parameters Block II (Surveillance) Block II (Armed)
Endurance 20 Hrs 12 Hrs
Service Ceiling 23,000 ft 21,000 ft
Max Speed 220 Kmph 220 Kmph
Wing Span 31 ft 31 ft
Data Link Range 300Km (LoS) 300Km (LoS)
Data Link Range (SATCOM) 1500Km 1500Km
Weapon System Not applicable Total 4 AGMs. 2x AGMs of 45kg under each wing station

Main Features
  • Improved Aerodynamics & Structure
  • Enhanced Payload Options (i.e. COMINT / ELINT, SAR, EO/IR)
  • SATCOM capable
  • Mid-air Engine restart capability
  • Equipped with ATC transponder / Provision of IFF
  • Provision of internal Pilot
  • Enhanced propulsion system
  • Retractable Landing Gears
  • Asymmetric Landing

Weapons System (Shahpar II - Armed
  • In Armed configuration, UAV is equipped with total 4 AGMs. 2x AGMs / weapon of 45kg under each wing station
  • 3rd party AGM can also be integrated with Shahpar-II keeping in view carriage capacity, integration feasibility

TACTICAL UAV SYSTEM

UQAB NG is catapult launched, net recovered fixed wing tactical UAV system, designed to conduct real time day & night reconnaissance and surveillance missions while offering long endurance, high service ceiling and optimized RCS Signatures. It is a low weight and compact system ideal for real-time surveillance missions up to 150 km with 8 + hrs of endurance. The performance and capabilities of Uqab-NG makes it superior to any other conventional surveillance UAV. Uqab-NG has been precisely designed for the clients requiring an ultimate solution for their operational needs without any runway.


Specification
Launch / Recovery Hydro-pneumatic launch / Hoisted Net System & Emergency Parachute
Dimensions Wing Span:6.20m, Length: 4m
Range 150 km LOS
Endurance > 8hrs
Service Ceiling Up to 18000 ft AMSL
MTOW 100 + 5kg
Flight Controller Dual core DSP Processor, STIM MEMS IMU
Navigation RTK based Tri Constellation DGNSS,
Magnetic Compass based Dead reckoning
Day: 27.7x Optical Zoom, 1080p25 FHD
Video Sensor Ni: 14x Optical Zoom cooled
Payload IR, 640x512, 25 Hz Sensor
LRF: 12 km, Stability < 25prads
Target tracking
Al based Multiple Target Recognition
Geo referencing & pointing
Failsafe Auto Return to Base / land in case of low battery & link failure

Salient Features
  • Modular design for mobility & rapid deployment
  • Inbuilt redundancies & failsafe provision
  • HD day & cooled IR sensors
  • Intelligent target classification & tracking with geo referencing
  • Dual band encrypted Data / Video links
  • Stanag compliant GCS with operator consoles / eqpt & Datalink hardware
  • Mission playback & data-log

UAV System

Scout VTOL is a vertical takeoff & landing Mini UAV System having the hovering capability and requiring crew of 2 x personnel for Ops, offering Real-time Day and Night ISR capabilities. It is a Quad-Copter configuration with four brushless electric motors. The high number of motors gives the UAV requisite thrust to carry a payload of up to 2 kg. Scout-VTOL Mini UAV’s light weight and small size make it ideal for quick deployment and portability, giving users an extra edge.


Features
  • Day/Ni Intelligence, Surveillance & Reconnaissance Mission
  • Payload Dispensing / Delivery up to 2 kg
  • Complete Autonomous Operation with pilot override option
  • Modular, man portable
  • Handheld GCS consoles for AV & payload operator
  • Fast redeployment / turn over

Main Specifications
Airframe Quadrotor configuration, carbon fiber structure with detachable arms, man portable (single person), tool less assy
Range Endurance 5~7 km
>65 mins with Day / Ni ISR camera
> 40 mins with 2 kg additional payload
Service Ceiling Up to 3200 m AMSL
Wind Resistance < 14m/s
Take-off Weight 11 kg (65 mins for ISR)
13 kg (40 mins for payload dispensing)
Dimensions 1280x1280x500 mm
Payload Day: 30x Optical Zoom with 1km LRF, 1080p25
FHD Video
Ni: 640x480, 25 Hz, 13mm+52mm, 2x, 4x
Digital zoom
Telemetry Flt Modes, Voltage indicator, Signal strength, Flt Altitude / Attitude / Distance & Speed
Maps Offline, scanned & Google Maps
Failsafe Auto Return to Base / land in case of low battery & link failure



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

DAY / NIGHT SURVEILLANCE & TARGETING PAYLOAD

ZUMR - Ilis a high performance Multispectral Imaging payload with 24/7 Mission Capability with Enhanced Imagers. It is highly stabilized system with 2 LRUs (Line Replaceable Units)


Features

High performance Multispectral Imaging
24/7 Mission Capability with Enhanced Imagers
Low Weight and Small Size Highly Stabilized System
2 LRUs (Line Replaceable Units)


Missions

Tactical support
Aerial imagery
High performance EO/IR payload for precision munitions (LGB, Missile) delivery


Sensor Configuration
Enhanced Day Imager (Continuous Zoom)
Resolution 752 x 582
Field of View: Wide 24°H x 18°V
Narrow 0.7°H x 0.5°V
Zoom 34x (Optical)

Thermal Imager
Resolution 640 x 512 FPA
Field of View:

Battlefield Damage Assessment Search and Rescue, Tactical Support


Technical Characteristics

4 axis gyro stabilized system Azimuth 360° continuous Elevation 10° to — 110° Weight 49Kg


Power Requirement and Interface
Voltage 24-32 VDC
Power 400 W
(600 W max)
Video Interface Analog, PAL
Serial Interface RS232, RS422

Environmental

MIL-STD-810F
MIL-STD-461E


Wide 24.3°H x 19.5°V
Medium-Wide 4.0°Hx3.2°V
Narrow 1.26°H x 1.0°V
Super-Narrow 0.63°Hx0.5°V (E-Zoom)

Laser Designator
Range 20m -20Km
Energy >85mJ
Code NATO, Custom

Laser Pointer

NVG Compatible (0.7W)


Platforms

UAVs, Aircrafts, Helicopters, Naval Ships

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

Sensor Configuration

Tactical support
Aerial imagery
High performance EO/IR payload for precision munitions (LGB, Missile) delivery


Sensor Configuration
Day Camera HD
Resolution 1920 x 1080
Field of View:
Wide 63.7°H x 47.7°V
Narrow 2.39 Hx 1.7°V
Zoom 30x (Optical)

Spotter Scope/NIR HD
Resolution 1920 x 1080
Field of View:
Wide 24° H x13°V
Narrow 0.9° Hx 0.5°V
Zoom 27x (Optical)
  • Day and Night surveillance of-site (Offshore platforms, industrial and sensitive sites)
  • Border surveillance and homeland security
  • Tracking, Tactical support

Technical Characteristics

4 axis gyro stabilized system
Azimuth 360° continuous
Elevation 10° to — 110°
15 Kg
ø 10.5", Height: 16"


Power Requirement

Voltage 28 VDC
Consumption <200W


Environmental

MIL -STD-810F, MIL-STD-461E


Thermal Imager SD
Sensor 640 x 512 MCT
Field of View:
Wide 16°H A~ 12°V
Narrow 1.8°H A~1.35°V
Zoom 9x (Optical)

Laser Range Finder & Laser Pointer

Range 12KM max
LP (0.3W) NVG Compatible

Platforms

UAVs, Aircrafts, Helicopters Aerostats and Ground Based Vehicles for area monitoring

BURQ

Burq is a Semi Active Laser Guided Air to Ground Missile (AGM). It has the capability to precisely attack the enemy personnel, light and armored vehicles, bunkers and buildings with high integration level, superior fire accuracy and better reliability. The semi-active laser seeker and cutting-edge navigation technologies makes it exceptionally accurate and distinguished weapon system to precisely engage moving and static targets.


Performance Characteristics

Operational Specifications Range
Launch Altitude
Carrier Launch Speed
Max Missile Speed
Hit Probability		 2.5-8.0km
500 to 5000 meters (MSL)
150 to 220 km / hr
Mas < 1.1
> 90%
Physical Specifications Length
Diameter
Weight
 1450 mm
180 mm
≤ 45Kg
Storage Storage life 10 years in Standard Conditions
Laser Seeker Laser Wavelength
Laser Pulse Width
Pulse repetition frequency		 1064 nm
15+ 5ns
19 ~ 21Hz

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