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PWI | Pakistan Weapons Industry

MOFA-200A (Muti Option Fuze for Artillery)


DESCRIPTION

* Multi Option Fuze for Artillery that incorporates all the features of artillery fuzes.
* Multi Channel Harmonic Processing
* High noise immunity and low probability of cause of burst, by base-bleed motor burnout/ round vibrations
* No known jamming system in this frequency band i.e "S" band.
* Intelligent design.
* Freely available components.
* Inductively programmable in < 1.55 seconds.
* Micro controller based design.



FOUR MODES OF OPERATION


Proximity Mode: (three heights of burst)

* Burst height low 4m ± 2m
* Burst height medium 10m ± 5m
* Burst heights high 20m ± 9m

Time Mode:

* Programmable from 3 sec to 199.9 sec with 100 ms of increment.

Point Detonation Mode:

* Detonation on impact.

Point Detonation Delay Mode:

* Detonation with delay after impact
* Programmable delay (2 ms-50 ms).



PERFORMANCE SPECIFICATIONS

Artillery Round Interface All 105 mm, 130 mm and 155 mm projectiles with bursting munitions.
Gunfire Environment 30,000g&#8217;s maximum 18,000 RPM
Operational Environment -40oC to + 71oC
Mission Duration 200 seconds maximum
Height-of-Burst Accuracy All HOBs in 90% lethality range regardless of terrain or firing conditions
Time Mode Accuracy 0.1 second
Reliability >90%
Storage Life 20 years controlled, 2 years uncontrolled
MOFA-200A-02.jpg
 
ACMI (Air Combat Maneuvering Instrumentation System)


INTRODUCTION

Success in the modern air-to-air combat arena depends on effective and realistic peacetime training. The nature of peacetime training requires accurate and detailed mission debriefs. Accurate reconstruction of the mission events is a challenging aspect of the mission debrief. AERO has developed Air Combat Maneuvering Instrumentation System which has revolutionized the training concept of Air Force.

ACMI-01.jpg


SYSTEM CAPABILITIES


The ACMI system is designed to be range-less i.e. it can be operated without any restriction in any area. The system records the "Time Space Position Information" (TSPI) of all the aircraft involved in the training exercise along with their essential parameters onto a removable data storage. The important parameters are shared amongst participant's aircraft as well on ground for real time debrief. The capabilities of the system include:

* Acquisition of aircraft data (MIL-STD-1553 or RS-232 bus)
* Exchange of data between the participating aircrafts using real time data link .
* Capture of &#8220;Weapon Employment Events&#8221;&#8221; (release/firing command).
* Notification to pilots of weapon event results such as hit and miss for missiles for real time kill removal functionality.
* Real time warnings to the pilot such as collision kill/miss etc..
* Recording of time synchronized relevant information for post mission debriefing replay like chaff/flare dispenser, RWR, EW etc.
* Post Launch missile fly out and bombing accuracy calculations.



DEBRIEF STATION CHARACTERISTICS


The debrief ground station software consists of three major parts:

* Pre-mission configuration
* Debriefing and Mission Recreation.
* Report Generation and System Management.

Recreation of mission includes graphical regeneration of mission as well as providing of information in numerical form that is essential for carrying out an effective debrief.
ACMI-02.jpg


ACMI-03.jpg
 
MOHAFIZ (Chaff & Flare Dispenser System)


MOHAFIZ Counter Measures System is designed and produced for military aircraft and helicopter applications.



SYSTEM FEATURES


* Microprocessor based programmable system.
* Display of remaining chaff & flare cartridges.
* Four modes of operation: Trigger, Manual, Auto and Emergency.
* Interface with Radar Warning Receiver (RWR) and Missile Approach Warning System (MAWS).
* Misfire compensation.
* Ten programmable sequences for automatic dispensing of chaff and / or flare.
* Power-on-self-test and periodic built-in-test.



PRODUCT SYSTEM DEFINITION


Standard MOHAFIZ Counter Measures System:

* 1 x Display and Control Unit (DCU).
* 1 x Control Processing Unit (CPU).
* 2 x Fire Control Unit (FCU).
* 2 x Dispenser Unit comprising of 8 x Magazines (each magazine can carry 9 x Flare cartridges or 18 x Chaff cartridges).

Reduced Payload MOHAFIZ Counter Measures System:

* 1 x Display and Control Unit (DCU).
* 1 x Control Processing Unit (CPU).
* 1 x Fire Control Unit (FCU).
* 1 x Dispenser Unit.



FLARE CHARACTERISTICS


* Jamming Wavelength: 1.5 micron
* Peak static radiation intensity: >20 KW/Sr
* Flare rise time: < 0.25 sec
* Flare burn time: > 3.5 sec
* Initial ejection velocity: >25 m/sec



CHAFF CHARACTERISTICS


* Frequency range: 2 - 18 GHz
* RCS: 10 m2
* Chaff bloom time: < 500 ms
* Initial ejection velocity: 15 - 25 m/sec



MOHAFIZ SYSTEM


Mohafiz-03.jpg


Mohafiz-02.jpg
 
AVTR SYSTEM (Airborne Video Tape Recorder System)


Airborne Video Tape Recorder (AVTR) System is designed for recording of Head Up Display (HUD) / Sight View of combat / training aircraft and helicopter applications. The simplified two LRUs solution is adaptable to any Airborne Platform.



SYSTEM CHARACTERISTICS


* Monitor Head Up Display (HUD) / Sight View
* Monitor pilot Headphone Audio.
* Monitor the event when Weapon Release Button is pressed.
* Convert the monitored visual, audio and event mark information into PAL/NTSC format electronics signal.
* Record visual, audio and event mark PAL / NTSC electronics signal into Digital 8 / Hi 8 video format.
* Automatically stops recording and indicates to the pilot when the tape ends or presence of dew is detected.
* Automatically switches on the heaters inside the recorder when the temperature is low enough to impair the video quality.
* Introduction of two layers of shock mounts provide protection against a wide range of low and high frequency vibrations.
* Adaptable for installation on any airborne platform due to its compact state of the art design.
* Simplified design consists of only two LRUs, Recorder and Camera & Control Panel Assembly.

AVTR-System-01.jpg


CAMERA & CONTROL PANEL CHARACTERISTICS


* Color CCD Camera of Resolution 752 x 582 (450 TVL)
* Integrated control panel provides control of the whole system.
* Provides status and error indication to the pilot.
* Provides video in PAL / NTSC Format.
* Field of view is 22o Horizontal and 16.5o Vertical.
* Auto Iris lens enhances the capability of the camera to provide best quality video in different light conditions.
* Designed according to the installation platform.



RECORDER CHARACTERISTICS


* Records Video in Digital 8 / Hi 8 Format
* Recording Time.
* Digital 8 Format: 90 minutes in Short Play (SP) Mode, 135 minutes in Long Play (LP) Mode.
* Hi 8 Format: 150 minutes maximum.
* Operating Temperature Range: -55o C to +70o C.
* Dimension: 172 x 130 x 204 mm.

AVTR-System-03.jpg


AVTR-System-02.jpg
 
LISA-4000 AHRS (Attitude & Heading Reference System)


Manufactured under co-production license from Northrop Grumman Italia (NGI). The Lisa-4000 performs two distinct basic functions:

* Flight Reference.
* Navigation.

The Flight Reference function provides:

* Heading and Attitude for Display/Autopilot.
* Anti-aliasing filtered body angular rate.
* Linear Acceleration data for autopilot inner loop stability augmentation.

Navigation is performed by coupling the LISA 4000 with a Doppler Radar and Air Data Computer or with a GPS. As a navigator the LISA-4000 also outputs high speed inertial velocity data required for accurate weapon release.

The LISA-4000 therefore provides all the inertial output parameters required for Autopilot, Navigation, Display and Weapon Delivery.
Lisa-07.jpg



CHARACTERISTICS


General:
* Size: 1/2 ATR Short/Short (322mm)
* Temperature: -40o C to +71o C
* Weight: 6.2 Kg
* Cooling: Not Required
* Power: 90 W, 18-32 Vdc

Outputs:
* Digital ARINC-429, MIL-STD-1553B, RS-422/485 (Heading, Attitude, Accelerations, Rates, Vertical Velocity)
* Synchro ARINC-407 (Heading, Pitch, Roll, Interlock for Autopilot),Eastern standard synchro output
* Analog (Yaw Rate, Validities)

Accuracy
* Heading: 0.8o
* Attitude: 0.5o
* Doppler/AHRS Navigation: < 1% Distance Traveled, GPS 80m CEP.



SYSTEM INTEGRATION FEATURES


* Openess, Modularity and Scalability for a real Integration.



OPITIONAL LRU&#8217;S PACKAGAE

CCMU-Automatic Flux Value Calibration.
Lisa-01.jpg



DCP-Full Digital autonomous interface control.
Lisa-02.jpg


SBU-Eastern Avionic Integration.
Lisa-03.jpg


ENHANCE AVIONICS PACKAGE

ADI/HIS-Fit & Form Cockpit retrofit with enhanced functions.
Lisa-04.jpg


MISSION COMPUTER-In flight/on ground management of large databases, flight plans, missions.
Lisa-05.jpg


MAPS DISPLAYS-Several overlayed digital maps for navigation, Terrain & Obstacle Awareness.
Lisa-06.jpg


INTEGRATED SYSTEMS


* GPS.
* DOPPLER RADAR
* AIR DATA COMPUTER
* TACAN
* HEAD UP DISPLAY
* WEAPON DELIVERY COMPUTER
* AUTOPILOT
* VOR/ILS
* BEZO BALL

Lisa-09.jpg
 
DETONICS


At AERO we have the facilities of designing, development and production of different detonics, boosters, impulse cartridges, delay cartridges and munitions for different types of fuzes and conventional weapons. We also carry out research and development on different conventional ammunition, explosives, propellets, pyrotechnics & carry out manufacturing of different types of explosive pellets for different types of Detonics and boosters.

IMPULSE CARTRIDGE I-28

* Impulse Cartridge I-28 type is used for jettisoning / release of stores from Mirage Aircraft.



CHARACTERISTICS


Electrical Specifications:

* Normal Firing Voltage: 27 ± 2 V DC
* Safe current ( Max. No-fire Current ): 0.85 + 0.05Amp. For one minute
* Min. all fire current: 1.4 + 0.1 Amp.
* Normal Firing Current: 3.0 + 0.5 Amp.
* Initiator Resistance: 0.40 ~ 0.60 Ohms
* Energy Output: 2000 ~ 3000 Joules
I-28-02.jpg

Performance parameters:

* Pressure: &#8805; 80 bars
* Initiator I-28 ignition Time: &#8804; 85 ms
* Primer Firing Time: &#8804; 15 ms
* Storage Temperature: -40o C to + 65o C.

Product Life

The following life limits are assessed for AERO's Impulse Cartridge I-28 under ambient storage conditions.

* Shelf Life: 8 years
* Utilization Life: 5 years

I-28-01.jpg
 
DETONICS


At AERO we have the facilities of designing, development and production of different detonics, boosters, impulse cartridges, delay cartridges and munitions for different types of fuzes and conventional weapons. We also carry out research and development on different conventional ammunition, explosives, propellets, pyrotechnics & carry out manufacturing of different types of explosive pellets for different types of Detonics and boosters.

CARTRIDGE PPLT

* Cartridge PPLT is used in release unit/pylon of Mig-27 Aircraft.



CHARACTERISTICS

PPLT-02.jpg

Electrical Specifications:

* Safe Current at 28 VDC: 0.80 Amp
* Minimum Firing Current at 28 VDC: 1.50 Amp
* Normal Firing Current at 28 VDC: 3.0 Amp
* Electrical Resistance: 0.4 ~ 0.6 ohm

Performance parameters:

* Peak Pressure: (i) 25.0 ~ 32.0 bars at +21o C & -40o C. (ii) 26.0 ~ 35.0 bars at + 93o C
* Ignition Time: not more than 90 ms

PPLT-01.jpg


---------- Post added at 07:58 PM ---------- Previous post was at 07:57 PM ----------

DETONICS


At AERO we have the facilities of designing, development and production of different detonics, boosters, impulse cartridges, delay cartridges and munitions for different types of fuzes and conventional weapons. We also carry out research and development on different conventional ammunition, explosives, propellets, pyrotechnics & carry out manufacturing of different types of explosive pellets for different types of Detonics and boosters.

CARTRIDGE TD-19PK

* Cartridge TD-19PK is used for jettisoning / release of stores from F-7 Series Aircrafts.



CHARACTERISTICS


Electrical Specifications:

* Normal Firing Voltage: 27 ± 2 V DC
* Safe current (Max. No-fire current): (0.7 + 0.05 amp at 27 ± 2 V DC)
* Min. all fire current: (1.5 amp at 27 ± 2 V DC)
* Normal Firing current: 3 + 0.5 Amp.
* Initiator Resistance: 0.30 ~ 0.55 &#937;.

Performance parameters

* Pressure: 150 ~ 170 bar
* Ignition Time: not more than 85 ms
* Primer Firing Time: < 15 ms

Storage Temperature

* -40 oC to +60 oC

Product Life

The following life limits are assessed for AERO's Cartridge TD-19PK under ambient storage Conditions.

* Shelf Life: 10 years
* Utilization Life: 3 years

TD-19PK-01.jpg





DETONATOR ELECTRIC To 10/20


This detonator is initiated by electric pulse and filled with sensitive initiatory compositions and secondary explosives.



CHARACTERISTICS


* Resistance range: 2.8 to 3.8 &#937;
* Response time: &#8804; 10 micro second
* Detonator type: Bridge wire
* Safe current: 235 milli Amp.
* Firing current: 600 milli Amp.

Sensitivity 1micro farad capacitor charge to 50 V should cause functioning in &#8804; 10 micro sec. All processes involved in the manufacturing of this detonator are controlled according to ISO: 9001- 2000 accreditation resulting into safe working practices through rigorous risk assessments.



APPLICATION


* TO 10/20 electric detonator initiates explosive train of AB-Series electronic fuzes when desired electric pulse is applied.

DE-1020-01.jpg



DETONATOR M-35

DESCRIPTION M-35 is a non electric detonator and is filled with primary and secondary explosives. This detonator is initiated by an electric detonator and used to initiate the booster charge in explosives train. All processes involved in the manufacturing of this detonator are controlled according to ISO: 9001- 2000 accreditation resulting into safe working practices through rigorous risk assessments. APPLICATION * M-35 detonator is used in different types of fuzes and forms explosive train

D-M-35-01.jpg



CUP BOOSTER


DESCRIPTION

Cup Booster is filled with secondary explosive pellets and used to explode main explosive booster charge. Boosters of different Explosive densities are being manufactured. All processes involved in the manufacturing of this cup booster are controlled according to ISO: 9001- 2000 accreditation resulting Into safe working practices through rigorous risk assessments.

CB-01.jpg



ADAPTER BOOSTERS M-148/M-147

DESCRIPTION These Adapter boosters are filled with C.E explosive pellets and are used to explode main explosives charge of General Purpose Steel & Pre-Fragmented Bombs. Density of explosive pellet is maintained as per requirements. All processes involved in the manufacturing of these adapter boosters are controlled and according to ISO: 9001- 2000 accreditation resulting into safe working practices through rigorous risk assessments. The adapter booster M-148 is used in nose while adapter booster M-147 is used in tail of General Purpose Bombs.


AB-M148-M-147-01.jpg
 
RABTA (C4I/ Air Defence Automation System)


A complete C4I system, that can interface all types of sensors (radars, sonars, IR sensors etc), to form a self-healing self-forming intelligent network. System supports upward, downward and lateral flow of information to bring all tiers of command at the same level of situational awareness. The system can interface to weapons as well, to pass on firing and control orders automatically.



RADAR INTERFACE & DAQ SYSTEM


The system is designed to acquire radar targets information present in the form of video/plot/track. For extracting this information, system supports a multitude of protocols (e.g., synchronous, asynchronous), electrical standards (e.g., RS-485, RS-422, RS232). System is configurable to receive target data from any standardized/known format.



RADAR DATA EXTRACTOR


Radar Data Extractor (RADEX) extracts digital target information by processing primary radar video. The RADEX is designed to accommodate variable scan rates and signal bandwidths of both short and long-range radars and utilize both normal and MTI video signals. It detects targets by correlating target 2-D profile with pre-stored profile. It precisely locates a target by finding maximum strength of radar video in a configurable 2-D region depending on time on target. All processing functions are fully configurable to adapt to specific customer needs. The main characteristics of RADEX include:

* 14-bit sampling at 0.25 Mhz to 20Mhz (max).
* Processing Channels: I/Q / MTI / Normal Video Processing.
* Dynamic Clutter Mapping.
* Target Capacity: 1600 Targets per Scan.



IFF DECODER
Rabta-04.jpg

IFF Decoder provides digital target extraction for all ICAO and AIMS compliant interrogators. IFF Decoder interfaces directly to control centers or other downstream processors. In addition to providing high quality digital secondary target reports, IFF Decoder also correlates primary radar information from Radar Data Extractor.Main features of the decoder are:

* Processing Modes: 1,2,3/A and 3/C.
* IFF Video Sampling: Digital sampling at 4Mhz &#8211; 10Mhz (Max).
* IFF Video Processing: Digital/Analog IFF video processing
* Target Capacity: Up to 1600 reports per scan..
* Garbling Detection and resolution of both super imposed and interleaved target returns.
* Performs in the densest FRUIT environments through defruiting techniques.


Rabta-06.jpg

RADAR DISPLAY CONSOLE (RDC)

AERO's Radar Display Console is a fully functional field proven Radar Display with powerful control features for the controllers/operators of the radar. Its integration with variety of radars is field proven. It can display raw radar video as well as processed target information.The numerous display settings/control features allow the controller/operator efficient air-space-management through Radar Display Console.
It has the following technical characteristics:

TECHNICAL CHARACTERISTICS
Rabta-05.jpg

RAW VIDEO:
* Display of multiple videos in separate colors
* User configurable intensity control for all types of videos

PLOTS:
* IFF and fused plots have further classifications according to the military and civil aviation standards.

TRACKS/TRACKER TARGET DATA:
* Different types of targets (output from Multiple Radar Tracker) are displayed on the screen in accordance with MIL-STD-2525B.

BEARING LINES:
* User configurable Plot Suppression Areas and Video Suppression Areas in multiple shapes.

SYMBOLS:
* User can insert/remove different type of symbols of military importance

INTERCEPTION PROFILE GENERATION:
* Controllers/operators can generate interception profiles for the actual interception that is being carried out for the fighter aircrafts or for mock interceptions for training purposes.
* The fighter & target parameter information such as speed/heading/angles of turn etc are also calculated internally by the system upon each track update and are shown to the user.




VOICE SWITCHING SYSTEM (VSS)

Rabta-07.jpg

Voice Switching System is designed to provide highly reliable, state-of-the-art, air-to-ground,ground-to-ground, and intercom communications for controllers of Military and civil air traffic; Air-to-ground communication interfaces provide connectivity between UHF, VHF and HF radio transmitters and receivers; Ground-to-ground communication interfaces provide connectivity to the public switched telephone network (PSTN), the defense switched network, long haul leased telephone lines, and the base telecommunications infrastructure; human interface to the communications network for safe and efficient communication control; each operator has the control to switch between any of the available radio and telephone channels; The Graphical User Interface (GUI) provides a flexible user configurable and friendly control.



MULTIPLE RADAR TRACKER (MRT)


* Can handle up to 2000 system tracks simultaneously.
* Can track maneuvers of up to 7 sustained Gs.
* Kalman filter based prediction engine.
* Dual mode association using both Nearest Neighbor (NN) and Joint Probabilistic Data Association (JPDA) algorithms.
* Provides option to force fuse tracks manually.
* Facilitates to exchange labels and change ids of tracks as desired.



AIR SITUATION DISPLAY (ASD)
Rabta-08.jpg


* Compliant with mil-std-810E for anti-shock, anti-dust and weatherproof design.
* Compliant with mil-std-461 for electromagnetic interference.
* Mil-std-2525 compliant C4 I display with complete GIS support.
* Software can handle upto 2000 Tracks,2000 Symbols and 65535 vector areas simultaneously.
* Up to 255 vector maps can be overlayed simultaneously.
* Automatic interception profile generation feature to facilitate GCI operation.



THREAT EVALUATION AND WEAPONS ASSIGNMENT


Threat Evaluation and Weapons Assignment (TEWA) is an intelligent system designed to evaluate threats and engage weapons to these threats. TEWA detects hostile tracks and assigns a threat level to them. It determines all vital points and areas and calculate their threat scores and sorts out all those weapons that can engage these threats and assigns weapons to these threats.

FEATURES:

* Provides automatic air situation assessment.
* Warns system for incoming hostile tracks.
* Performs automatic threat evaluation and calculates threat level of these hostile tracks.
* Determines suitable weapons that can be used to engage these hostile tracks and engage appropriate weapons to these hostile tracks
* Guides fighters for interception.


WAR GAMING SYSTEM:

* An Air Defence war gaming system based on real-time adversarial head-to-head paradigm.
* Scalable architecture allows easy addition of new models.
* Recording and scenario saving options to facilitate review of player performance.
* Up to 255 players per team.
* Up to 255 referees to monitor the progress of the game.
* Integrated Threat Evaluation & Weapons Assignment module to facilitate tactics evaluation.



RADAR AUDIO VIDEO RECORDING SYSTEM


Radar Audio Video Recording System (RAVRS) is a device for automatic recording, storage and replay of the video information coming from radar as well as the voice information coming from multiple sources. RAVRS is a state-of-the-art technology in the field of digital data logging. It is a powerful system, designed to meet the growing needs in mission critical systems, of reliable audio and video recording.

TECHNICAL CHARACTERISTICS:

* 24 hours a day recording of digital radar video and audio data.
* Fast search of recorded data.
* Simultaneous recording and playback facility.
* Data archiving on internal hard disk (HDD) and external media (DVD-RAM).
* Synchronous playback of the multiple audio and video channels.



BASE OPS ROOM / FIC SOFTWARE


FEATURES:

* Two-way communication of tactical and operational data.
* Tabular display on remote and central command center.
* Handling of thousands of records simultaneously.
* Communication mediums can be dialup, leased line and hot lines.
* Time synchronization with external source and record's time stamping.
* System can be installed at ground stations, ships and air-crafts.
* Encryption is used for secure data transfer.
* Auto acknowledgment mechanism implemented to assure the data communication.
* Can be interfaced with any existing database.
* Cost-effective solution.


Rabta-09.jpg
 
MAHFOOZ (Secure Communication Equipment)

Mafooz-05.jpg

MAHFOOZ (AERO-SCE) is an indigenously developed secure communication system with space domain algorithm. Implemented in specifically designed secure hardware, supports voice, fax and data communication on public switched telephone network and compatible networks.



KEY FEATURES


* AERO-SCE provides a real time, full duplex implementation of the most modern cryptographic techniques that have proven to be efficacious in numerous evaluations.
* Indigenously developed 128 bit customizable encryption algorithm with proven security strength.
* True independent dual security layers due to incorporation of 571 bit elliptic curve cryptography.
* Proprietary multi source frequency domain hardware random number generator.
* Encryption is performed in a tamper proof hardware module with secret algorithms profiled by the security manager.
* Specifically designed to encrypt voice, fax and computer data over PSTN and its compatible networks.
* Intelligible voice quality with good speaker recognition.
* Simple installation by merely connecting the unit between PSTN line and Phone Set.
* Operates like a normal telephone set in insecure mode.
* Key filling through electronic key fill device with encrypted contents.
* Flexible hardware to incorporate any customized encryption algorithm.



SYSTEM SPECIFICATIONS


Physical:
* Mounting: Desktop. 10&#8221; x 8&#8221; x 3&#8221; (L x W x H)
* Weight: less then 3kg
* Display: 2-line LCD
* Keypad: Customized silicon rubber

Communication:
Oparable on all PSTN and Compatible networks
* Modem: V.92 Compatible with auto fallback
* Data Rates: From 19.2kbps to 2.4 kbps for data & Fax.
* Synchronization Time: 15-20s (Depending upon line condition)
* Process Delay: less then 100ms
* Voice Quality: GOOD
* Fax Compatibility: All G3 Standard fax Machines
* Data Compatibility: Transparent; All Standard UART interface at 9600bps, 8, N, 1 Supports various file extension data transfer e-g. .jpg, .RAR, .zip, .PDF, .txt, doc, .PPT etc

Interfaces
* Telephone: RJ-11
* Data: PC Standard DB-9
* Fax: RJ-11
* Power: 2.5mm DC barrel connector

Environmental
* Operating Temperature: -10o C to + 50o C
* Storage Temperature: 120o C to 65o C
* Casing: Metallic, Splash protected
* Humidity: 95% non-condensing
* Vibration: Mil-Std-810F, Method 514.5

PCBs
* Multi-layer design up to 10 layers
* Component Density: More then 250 types of components with wiring Density UP to 0.07962mm

Mafooz-04.jpg



CRYPTOGRAPHIC SPECIFICATION


* Non public domain, customizable algorithm.
* Master key length, 512 bit
* Key storage capacity of 500 different Keys of 512 bit each
* Algorithm execution and Key storage on single BGA chip with Specialized PCB design to avoid on board tempering
* Key management using electronic key gun device
* True independent dual layer of system security
* Multi-source, frequency domain hardware random number generator
* Smart card based device authentication System
* Temper proof casing



STANDARD COMPLIANCE


* SCE Encryption algorithm operates in CBC mode in Compliance to NIST-PUB-800-38A
* Data integrity provided by MAC in Compliance to FIPS-PUB-198A
* Multi-source hardware random numbers acquisition mechanism in Compliance with FIPS-PUB-180-2
* Session secret key ECC based Key exchange protocol in Compliance to FIPS-PUB-186-2
 
This thread is insane. i have gone over page 1 and it took me 4 hours.... This is a gold mine... Imran, great great work !!! you should be give a title of researcher....

Now on the capability, Pakistan is done well for its small economy. Next generation wars are all about technology, and i am sure Pakistan is among the leaders when it comes to producing high class weapons !!! :tup:
 
Rocket 122 MM He (MBRL) YARMUK
Rocket 122mm HE (MBRL) is a ground to ground free flight artillery rocket fired from multi-tube or single-tube launcher. It is used against pesonnel and light material, providing both fragmentation and blast effect.

ROC_122MMHEMBRLYARMUK.jpg


TECHNICAL DATA
Calibre 122 mm
Weight of filled warhead 18.4 kg without fuze
19.4 Kg with fuze
Weight of propellant 20.4 kg double base
Total length of rocket 2,875 mm
Weight of complete rocket 66 Kg (approx)
Weight of bursting charge 6.0 Kg Compo B
Performance
Muzzle velocity 400 metres/sec
Max. time of flight 78 sec
Range of rocket 20 Km
Max. range without brake ring 20,580 metres
Max. range with small brake ring 15,890 metres
Max. range with large brake ring 12,080 metres
 
This thread is insane. i have gone over page 1 and it took me 4 hours.... This is a gold mine... Imran, great great work !!! you should be give a title of researcher....

Now on the capability, Pakistan is done well for its small economy. Next generation wars are all about technology, and i am sure Pakistan is among the leaders when it comes to producing high class weapons !!! :tup:

yaar i dont wanna be some thing else and then everyone will ask me qes :lol:

buttttttttttttttt this thread should be sticky damn its pride made in pakistan :hitwall:

is main kya pesy lagty hain ?:angry:
 

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