الصناعة العسكرية الباكستانية

رد: الصناعة العسكرية الباكستانية

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رد: الصناعة العسكرية الباكستانية

ممتاز الله يزيدكم ويبارك لكم
 
رد: الصناعة العسكرية الباكستانية

شكرا اخي بارك الله فيك على الموضوع الرائع
بالتوفيق والمزيد من التقدم لباكستان
 
رد: الصناعة العسكرية الباكستانية

الله يزيد و يبارك في باكستان الاسلام
 
رد: الصناعة العسكرية الباكستانية

ما شاء الله اللهم أحفظ الأسلام والمسلمين
تخيلوا أخوانى لو حدث تحالف بين مصر والسعوديه وباكستان بما لديهم من خبره فى الصناعات العسكريه سيكون العائد كبير جدا لكل الأسلام والعرب
 
رد: الصناعة العسكرية الباكستانية

[FONT=Geneva, Arial, Helvetica, sans-serif]BAAZ AERIAL DRONE[/FONT]
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[FONT=Geneva, Arial, Helvetica, sans-serif]Type [/FONT]
[FONT=Geneva, Arial, Helvetica, sans-serif]Recoverable aerial target.[/FONT]

Type
Recoverable aerial target.
Development
Designed for use with air defence guns and short-range SAM systems; system includes optical tracking facilities.
Airframe
Simple high-wing monoplane, with parallel chord wings and horizontal tail; GFRP fuselage, epoxy laminated polystyrene wing. No landing gear.
Mission payloads
Cannot carry mission pay load
Guidance and control
Radio command, by seven-channel VHF/FM transceiver. Transmitter power 9.6 V at 1.2 Ah; RF output 1 W; rechargeable battery. Receiver power 6 V at 1.2 Ah; rechargeable battery. Transceiver has two built in fail safe devices. If transmitter fails, engine shuts down after 1.5 seconds; if power fails or receiver malfunctions for any reason, including projectile strikes, an independent auxiliary power supply automatically operates the same fail-safe sequence.
Launch
By bungee powered catapult. Set up time 20 minutes; turnaround time 5 to 10 minutes
Recovery
Direct landing on reinforced belly, or parachute retrieval
Operational status
In production and service
Customers
Royal Saudi Air Force & Pakistan Armed Forces
Specifications
Power plant
One 100 cc (British Origin) two stroke engine with electronic ignition; two blade propeller. Fuel is 20:1 petrol/oil mixture.
Dimensions
Wing span 2.44 m (8 ft 0.0 in)
Length overall 2.10 m (6 ft 10.7 in)
Weights
Max launching weight 19 kg (41.9 lb)
Performance
Max level speed 113 kt (209 km/h; 130 mph)
Max range: visual 1.1 n miles (2 km; 1.2 miles)
Optical 1.9 n miles (3.5 km; 2.2 miles)
Max endurance 35 min
Prime contractor
Pakistan Aeronautical Complex (PAC), Aircraft Manufacturing Factory Kamra
[FONT=Geneva, Arial, Helvetica, sans-serif]Development[/FONT]
[FONT=Geneva, Arial, Helvetica, sans-serif]Designed for use with air defence guns and short-range SAM systems; system includes optical tracking facilities.[/FONT]
[FONT=Geneva, Arial, Helvetica, sans-serif]Airframe[/FONT]
[FONT=Geneva, Arial, Helvetica, sans-serif]Simple high-wing monoplane, with parallel chord wings and horizontal tail; GFRP fuselage, epoxy laminated polystyrene wing. No landing gear. [/FONT]
[FONT=Geneva, Arial, Helvetica, sans-serif]Mission payloads [/FONT]
[FONT=Geneva, Arial, Helvetica, sans-serif]Cannot carry mission pay load [/FONT]
[FONT=Geneva, Arial, Helvetica, sans-serif]Guidance and control [/FONT]
[FONT=Geneva, Arial, Helvetica, sans-serif]Radio command, by seven-channel VHF/FM transceiver. Transmitter power 9.6 V at 1.2 Ah; RF output 1 W; rechargeable battery. Receiver power 6 V at 1.2 Ah; rechargeable battery. Transceiver has two built in fail safe devices. If transmitter fails, engine shuts down after 1.5 seconds; if power fails or receiver malfunctions for any reason, including projectile strikes, an independent auxiliary power supply automatically operates the same fail-safe sequence. [/FONT]
[FONT=Geneva, Arial, Helvetica, sans-serif]Launch [/FONT]
[FONT=Geneva, Arial, Helvetica, sans-serif]By bungee powered catapult. Set up time 20 minutes; turnaround time 5 to 10 minutes [/FONT]
[FONT=Geneva, Arial, Helvetica, sans-serif]Recovery[/FONT]
[FONT=Geneva, Arial, Helvetica, sans-serif]Direct landing on reinforced belly, or parachute retrieval [/FONT]
[FONT=Geneva, Arial, Helvetica, sans-serif]Operational status [/FONT]
[FONT=Geneva, Arial, Helvetica, sans-serif]In production and service [/FONT]
[FONT=Geneva, Arial, Helvetica, sans-serif]Customers[/FONT]
[FONT=Geneva, Arial, Helvetica, sans-serif]Royal Saudi Air Force & Pakistan Armed Forces [/FONT]
[FONT=Geneva, Arial, Helvetica, sans-serif]Specifications[/FONT]
[FONT=Geneva, Arial, Helvetica, sans-serif]Power plant [/FONT]
[FONT=Geneva, Arial, Helvetica, sans-serif]One 100 cc (British Origin) two stroke engine with electronic ignition; two blade propeller. Fuel is 20:1 petrol/oil mixture. [/FONT]
[FONT=Geneva, Arial, Helvetica, sans-serif]Dimensions [/FONT]
[FONT=Geneva, Arial, Helvetica, sans-serif]Wing span 2.44 m (8 ft 0.0 in) [/FONT]
[FONT=Geneva, Arial, Helvetica, sans-serif]Length overall 2.10 m (6 ft 10.7 in) [/FONT]
[FONT=Geneva, Arial, Helvetica, sans-serif]Weights [/FONT]
[FONT=Geneva, Arial, Helvetica, sans-serif]Max launching weight 19 kg (41.9 lb) [/FONT]
[FONT=Geneva, Arial, Helvetica, sans-serif]Performance [/FONT]
[FONT=Geneva, Arial, Helvetica, sans-serif]Max level speed 113 kt (209 km/h; 130 mph) [/FONT]
[FONT=Geneva, Arial, Helvetica, sans-serif]Max range: visual 1.1 n miles (2 km; 1.2 miles) [/FONT]
[FONT=Geneva, Arial, Helvetica, sans-serif]Optical 1.9 n miles (3.5 km; 2.2 miles) [/FONT]
[FONT=Geneva, Arial, Helvetica, sans-serif]Max endurance 35 min [/FONT]
[FONT=Geneva, Arial, Helvetica, sans-serif]Prime contractor [/FONT]
[FONT=Geneva, Arial, Helvetica, sans-serif]Pakistan Aeronautical Complex (PAC), Aircraft Manufacturing Factory Kamra[/FONT]
 
رد: الصناعة العسكرية الباكستانية

[FONT=Geneva, Arial, Helvetica, sans-serif]ABABEEL AERIAL DRONE[/FONT]
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[FONT=Geneva, Arial, Helvetica, sans-serif][FONT=Geneva, Arial, Helvetica, sans-serif]T[/FONT][/FONT][FONT=Geneva, Arial, Helvetica, sans-serif]ype
Small arms target.
Development
Designed as all-arms air defence target for use with small arms and machine guns. Also used as basic trainer for operators of the larger and faster Baaz (which see).
Airframe
Small, simple high-wing monoplane with GFRP fuselage and a polystyrene foam, epoxy laminated wing. Full span flaperons and elevator; no rudder. Current models have increased fin area and less tapered wings. No landing gear.
Mission payloads
Cannot carry mission pay load
Guidance and control
Radio command (four-channel VHF transceiver). Transmitter power 9.6 V at 1.2 Ah; RF output 1 W. Receiver power 6 V at 1.2 Ah. Rechargeable battery. Ground support equipment consists of a box containing a 2.5 litre (0.66 US gallon; 0.55 Imp gallon) fuel container, electric engine starter, ammeter, 12 V battery to power equipment, and a selection of hand tools.
Launch

Hand-launched
Recovery

Belly landing on any reasonably level terrain
Operational status
In production and service
Customers

Royal Saudi Air Force & Pakistan Armed Forces
SpecificationsPower plant
One 0.9 kW (1.2 hp) 10 cc glow-fuel engine with two-blade propeller. Fuel capacity 0.38 litre (0.10 US gallon; 0.08 Imp gallon).
Dimensions

Wing span 1.60 m (5 ft 3.0 in)
Length overall 1.41 m (4 ft 7.5 in)
Tailplane span 0.60 m (1 ft 11.6 in)
Weights

Max launching weight 2.8 kg (6.2 lb)
Performance

Max level speed 75 kt (140 km/h; 87 mph)
Endurance 20 min
Prime contractor

Pakistan Aeronautical Complex (PAC), Aircraft Manufacturing Factory Kamra
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رد: الصناعة العسكرية الباكستانية

طراز الجديده صاروخ نصر باكستانيه

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IRTS صناعه باكستانيه

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شبكه تمويه صناعه باكستانى

made by Pakistan Air Weapon Complex.

Description

* Provides effective concealment of land platforms from surveillance methods by reducing their thermal signature.
* Light-weight: rapidly and noiselessly deployed and removed.
* Water-repellant, weather-proof and fire-resistant.
* Strong, non-rip material ensuring long service-life.

camouflage characteristics


* Anti-Visual
* Anti-Night Vision
* Anti-Infra-red
* Anti-Radar
* Anti-Millimeter Wave

mechanical characteristics


* Size Customized
* Available Colors Desert sand & grass (double-sided)
* Weight Nominal 240 g/m2
* Thickness Nominal 300 µm
* Tensile Strength (typical)
Warp 1700N/50 mm
Weft 1500N/50 mm
* Tear Strength (typical)
Warp 80N
Weft 100N

technical characteristics

* Base Fabric classified
* Coating classified
* Temperature Stability -25°C to 80°C
* Fire Resistance Flame retardant
Storage Life >10 years (dry, <50°C)

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Vehicle under the Net cannot be detected by a Thermal camera (Day time)
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Vehicle under the Net cannot be detected by a Thermal camera (Night time






برنامج صناعه اواكس مشتركه


باكستان و صين وقع صفقه 278 مليون دولارلصناعه اواكس جديد باسم ZDK-03 و نقل تقنيه الى باكستان هناك احتمال اول اواكس استسلم باكستان في نهايه 2010 و بعدين صناعه في باكستان على طائرات صينى بدل ما نظام روسي التى استخدمت صين في اواكس سابقه. ايضا حسب صفقه باكستان عنده خمسون في مئه حقوق الملكيه برنامج للبيع بلاد اخرين كذي الجى اف 17 - اف سي -1. ZDK-03 نقل معلومات مع الجى اف -17 و جيان -10 باكستانى .

http://www.allvoices.com/contributed...eal-with-china

صوره برنامج اواكس صيني باكستانى ZDK-03مشترك AESA على طائرات صينى Y-8F600

اثنين منهم دخلت في في الخدمه الباكستانيه

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Pakistan Develps air-burst A-P round

Pakistan Ordnance Factories (POF) has developed an air-burst anti-personnel round for the locally produced derivative of the Russian RPG-7, writes Doug Richardson. The new RPG-7AP has a warhead that contains 850 steel balls packed around a high-explosive charge.

It has a maximum range of 1,500 m and, according to the POF, is designed "to kill soldiers and damage equipment within 15 metres' radius".

In general configuration, it closely resembles the Type 69 40 mm air-burst anti-personnel grenade that China has developed for its Type 69-1 40 mm anti-tank grenade launcher. Like the Chinese round, it is propelled upwards by a jump mechanism when it strikes the ground. Once it reaches a height of about 2 m, the warhead detonates, scattering its steel balls.

The main difference between the Pakistani and Chinese rounds is that the muzzle velocity of the former is 95 m/s, slightly lower than the 102 m/s of its Chinese equivalent. Projectile weight is slightly higher - 2.85 kg rather than 2.8 kg - while the payload contains 850 steel balls rather than about 800.

Although the POF cites a calibre of 40 mm compared with the 75 mm of the Chinese round, in practice the Pakistani figure refers to the calibre of the launcher rather than the diameter of the warhead. The latter is about 75-80 mm in diameter.

Jane's Missiles and Rockets - Precision guided news and analysis

باكستان تقدم المتفجر جوا ألف ف الجولة

باكستان المصانع الحربية) وقد وضعت جو المضادة للأفراد انفجر المستديرة للالمنتجة محليا مشتق من الروسية ار بي جي 7 ، وكتب دوغ ريتشاردسون. آر بي جي جديدة 7AP يحمل رأسا حربيا الذي يحتوي على 850 كرات الصلب معبأة في جميع أنحاء رفيع عبوة ناسفة.

ويبلغ اقصى مدى من 1،500 م ، وفقا لميناء الفجيرة ، تم تصميم "لقتل الجنود والمعدات الضرر في غضون 15 مترا' دائرة نصف قطرها ".

في التكوين العام ، فإنه يشبه من نوع 69 عيار 40 ملم الجوية المضادة للأفراد انفجار قنبلة يدوية ان الصين قد تطورت لنوع 69-1 40 ملم مضاد للدبابات وقاذفة قنابل. مثل الدور الصيني ، فمن القذائف صعودا من خلال آلية القفز عند وقوعها على أرض الواقع. عندما يصل ارتفاعها الى حوالى 2 متر ، وتفجير الرؤوس الحربية ، ونثر من كرات الصلب.

والفرق الرئيسي بين الجولتين الباكستانية والصينية هو أن سرعته في السابق هو 95 م / ثانية ، أي أقل قليلا من 102 متر / ثانية ليعادل الصينية. وزن القذيفة أعلى قليلا -- 2.85 كيلوغرام بدلا من 2.8 كجم) -- في حين أن حمولة تحتوي على 850 كرات من الصلب بدلا من نحو 800.

على الرغم من أن المصانع الحربية ويستشهد من عيار 40 ملم مقارنة مع 75 ملم من الجولة الصينية ، في ممارسة هذا الرقم يشير الى باكستان لاطلاق عيار بدلا من قطر الرأس. هذا الأخير هو حوالي 75-80 ملم قطرا.
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رد: الصناعة العسكرية الباكستانية

قنبله عنوديه من شركه جدز الباكستانيه

COMBINED EFFECT MUNITION

Category : Arial Bombs
Manufacturer : GIDS
Detail


Introduction

Area denial of the enemy has always been the requirement of all Air Forces. The Combined Effects Munitions (CEM) combines this area denial effect with anti- armor shape charge effect. This capability allows imprinting multi-dimensional damage to a variety of targets.
Combined Effects Munitions (CEM) consisting of Tactical Munitions Dispenser (TMD) containing Combined Effects Bomblets (CEBs) and Safety and Arming (S&A) device. CEM has multiple target kill capabilities.

Upon impact CEM detonation activates three kill mechanisms:

1. Anti-Personnel
Mild steel bomblet body having a warhead containing 150 steel balls for fragmentation.
2. Anti-Armor
Copper cone based shaped charge for armor penetration.

Operational Features
Upon release from the aircraft, CEM falls away from the launch aircraft to a safe separation distance. Initiation of the nose fuze detonator detonates linear shaped charge that splits the dispenser open along its full length on each side. The Combined Effects Bomblets (CEBs) are dispersed in a stabilized nose down form over the pre-planned coverage area. Ram air causes the vane of S&A to rotate at high rpm (approx.15, 500), which results in arming of CEBs. Upon impact, the detonation wave is transmitted to the booster pellet, which finally explodes the main charge of the CEB.
Physical Features
Weight: 490+10 lbs
Diameter: 13.20 inches
Area: 137inches square
Fin Span (closed): 17.2 inches square
Lug Spacing: 14 inches
Fuze Type: Electronic time based, nose mounted
Fuze Safety Features:

1. Air Sensor to check 220 knots
2. Electro-mechanical system for explosive train alignment

No. of Bomblets: 247
Bomblet Warhead: Anti Armor
Performance Specifications
Launch Speeds: 400-600 KTAS
Launch Altitude: 100 m (level)
Angle of Attack: 0 to 60 Degrees
Operational Temperature Range: -40 deg to +71 deg C
Environmental Qualification: As per MIL-STD-331 and MIL-STD- 801F
Carriage Qualification : Same as MK-20
Shelf Life: 20 Years
Targets: Armored Vehicles
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رد: الصناعة العسكرية الباكستانية

قنابل اسقاط الحره و موجهه من شركه جدز باكستانيه


GP Series Steel Bomb (NATO APPLICATIONS)

Category : Arial Bombs
Manufacturer : GIDS
Detail


1. General purpose bombs effective against all kinds of targets.
2. Give blast as well as fragmentation effect.
3. Low Drag design with high Length-to-Diameter Ratio.
4. Can be carried on NATO standard suspension systems.
5. Forged from seamless steel tube.
6. Filled with Compo 'B' explosive.
7. Inert filling can be used for training purpose.
8. Can be used in the following configurations:-
1. Low drag configuration : when installed with Conical Fin Assembly
2. High drag configuration: when installed with Retarded Tail Unit.
9. Can be fitted with the following types of fuzes:-
1. Mechanical Nose fuze M-904 or equivalent.
2. Mechanical Tail fuze M-905 or equivalent.
3. Ultra Quick Electronic Impact Nose Fuzes AB-100 (in low drag configuration) and AB-105 (in low or high drag configuration).
4. Electronic Proximity Nose Fuzes AB-103 (in low drag configuration) and AB-104 (in low or high drag configuration).
5. Electronic Long Delay Fuze AB-112.
6. Electrically Timed Fuzes FMU-81/B, FMU-139 A/B.
7. Electronic (Tail) Fuze FMU-54 A/B

GP-80WP (WARSAW APPLICATIONS)
Description

1. Includes Integral E.F.I Cable for interfacing the nose fuze to Russian aircraft pylons
2. General purpose bombs effective against all kinds of targets.
3. Give blast as well as fragmentation effect.
4. Low Drag design with high Length-to-Diameter Ratio.
5. Can be carried on WARSAW standard suspension systems.
6. Forged from seamless steel tube.
7. Filled with Compo 'B' explosive.
8. Inert filling can be used for training purpose.
9. Can be used in the following configurations:-
1. Low drag configuration: when installed with Conical Fin Assembly.
2. High drag configuration: when installed with Retarded Tail Unit.
10. Can be fitted with the following types of fuzes:-
1. Mechanical Nose fuze M-904 or equivalent.
2. Mechanical Tail fuze M-905 or equivalent.
3. Ultra Quick Electronic Impact Nose Fuzes AB-100WP (in low drag configuration) and AB-105WP (in low or high drag configuration).
4. Electronic Proximity Nose Fuzes AB-103WP (in low drag configuration) and AB-104WP (in low or high drag configuration).
5. Electronic Long Delay Fuze AB-112WP.
6. Electrically Timed Fuzes FMU-81/B, FMU-139 A/B.
7. Electronic (Tail) Fuze FMU-54 A/B.

1267073163_GP-Series-Steel-Bomb.jpg






قنابل تفجير في الجو اثنا اقاط من جدز باكستانيه


Pre-fragmented Bombs (NATO applications)

Category : Arial Bombs
Manufacturer : GIDS
Detail


1. New concept in optimizing the effectiveness of conventional bombs.
2. Outer casing manufactured from composite fiber.
3. Contains spherical steel balls which shoot out in all directions when the blast occurs.
4. Extremely effective against soft targets at great distances from the point of detonation.
5. 5 to 6 times more effective than a General Purpose Steel Bomb.
6. Filled with Compo 'B' explosive.
7. Inert filling can be used for training purpose.
8. Can be carried on NATO standard suspension systems.
9. High Length-to-Diameter Ratio for low drag design.
10. Can be used in the following configurations:-
1. Low drag configuration: when installed with Conical Fin Assembly.
2. High drag configuration: when installed with Retarded Tail Unit.
11. Can be fitted with the following types of fuzes:-
1. 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). For high drag optimum lethality, the Electronic Proximity Nose Fuze should be used to burst the bomb 2-12 m above the ground.

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رد: الصناعة العسكرية الباكستانية

انظمهC4I و الدفاع الجوي اسمها صناعه باكستانيه


C4I AND AIR DEFENCE AUTOMATION SYSTEM

Category : C4-1 Air Defence Automation System
Manufacturer : GIDS
Detail


The Air Defense Automation System has been indigenously developed by Air Weapons Complex (AERO). The designed system collects information from all Air Defense sensors and radars, processes it, converts it into a standard format and displays it in real time at any desired location. The system architecture is independent of space, time and communication medium. The Command and Control System provides an environment for multiple functions to operate on the same hardware platform and share data via a Local Area Network (LAN) or a Wide Area Network (WAN).
The System allows the Commander to a view a fused picture of his complete Area Of Responsibility (AOR). It is a compilation of data from all Air Defense sensors, combined with battle plan, projection overlays, and any other data that is available, including:
current locations and planned movement operations of ground, maritime and air units of friendly, neutral, and enemy forces generated features and projections (e.g. battle plans, operating zones).
Our engineers work closely with the customers to provide them customized, open, flexible and cost-effective solutions to their Air Defense Automation System requirements. AERO provides comprehensive Integrated Logistic Support (ILS) throughout the life cycle of the System.
SALIENT FEATURES

1. Seamless integration with C4I systems.
2. Network centric design allowing self-forming and self-healing network (user can enter or leave the network dynamically).
3. Complete Air Situation Display (ASD).
4. User friendly and compact Graphical User Interface.
5. The System can be operated in different modes (Operator, Commander etc.)
6. Personnel training under simulation mode.
7. Scenario recording and replay facility.
8. Communication with lower and higher command centers.
9. Advanced GIS support.
10. Multiple layer architecture (Display of multiple maps).
11. Map features e.g. map loading, map editing, map color changing etc.
12. Preset and programmable zoom buttons.
13. Display of Latitude/Longitude, Georef and Grid System.
14. True battlefield scenario support.
15. Display of track history during interception operation. User can switch on/off history of track.
16. Track symbol indicating its category.
17. Track type indicates the threat status of the track.
18. Tactical interception aids available.
19. Radar on/off option.
20. Aircraft Plot Suppression Area (PSA).
21. Non-automatic track initiation area.
22. Weapons (SAM/AAA) status monitoring.
23. Use of commercial technologies.
24. Ergonomically designed Command and Control Console.
25. Easy maintenance.

MULTIPLE RADAR TRACKER
Multi Radar Tracker (MRT) uses state-of-the-art tracking algorithms to detect and track all modern, fast and highly maneuverable targets, hence forming an integral part of C4I and Air Defense Automation System. It works effectively in high clutter environments and displays real time information for any command & control function. It can handle 2000 plots and 1000 tracks. This capability can be further enhanced due to scalable design of the Tracker. It can be integrated simultaneously with homogenous and heterogeneous radars.
The Tracker automatically initiates and reliably tracks maneuvering targets. The tracks initiation and maneuvering detection is enhanced with multiple sensors. The trackers update the display information at a high rate to form a true, accurate and complete Air Situation Display (ASD) for all air-defense and air-traffic control operations.

The main functions of the MRT algorithm include:

1. Inferring the presence of valid targets from a series of plots and tracks received from different radars.
2. Calculating optimally by the sensor the true trajectories of the target in presence of uncertainties imposed by the sensor as well as aircraft dynamics.
3. Recognizing and rejecting false targets.
4. Successfully tracking and predicting the optimal estimates of the target in the presence of clutter and false alarms.
5. Displaying target tracking information.
6. Forming correct association between tracks and observation from radars in different environment.
7. Successfully tracking the target during extreme conditions of fast maneuver, formations, miss detection, cross-overs etc.
8. Fusing information from multiple radars of different ranges, resolutions, scan times and other radars parameters.
9. Analyzing the influence of sensor modeling, radar processor design, and change of other system parameters on algorithm design.
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التعديل الأخير:
رد: الصناعة العسكرية الباكستانية

انظمه ACMI تحكم و تحاليل مناوره الجويه صناعه باكستانيه

AIR COMBAT MANEUVERING INSTRUMENTATION (ACMI)

Category : Air Combat Manuvering Instrumentation System
Manufacturer : GIDS
Detail


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 debriefs. AERO has developed Air Combat Maneuvering Instrumentation System which has revolutionized the training concept of Air Force.



SYSTEM CAPABILITIES

The ACMI system is designed to be range-less i.e. it can be operated without any restriction in any area. The 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.

SALIENT FEATURES

1. An effective training tool for combat pilots, used for digital recreation of a mission
2. Mission can be replayed in various modes
3. Installed on Mirage, F-7P, F7-PG & F-16 Aircraft
4. Specifications:
1. Real time transmission
2. 5 hrs recording on compact flash
3. Theatre environment
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رد: الصناعة العسكرية الباكستانية

انظمه تسجيل فيديو على متن طائرات مقاتلات صناعه باكستانيه من جدز


AIRBORNE VIDEO TAPE RECORDER

Category : Airborne Video Tape Recorder System
Manufacturer : GIDS
Detail


Introduction
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. The following are the characteristics of this system.
System Characteristics

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

Description

1. Color CCD Camera of Resolution 752 x 582 (450 TVL).
Integrated control panel provides control of the whole system.
2. Provides status and error indication to the pilot.
3. Provides video in PAL/NTSC Format.
4. Field of view is 22� Horizontal and 16.5� Vertical.
5. Auto Iris lens enhances the capability of the camera to provide best quality video in different light conditions.
6. Designed according to the installation platform.
7. Weighs less than 420 grams.
8. Records Video in Digital 8 / Hi 8 Format.

Recorder Characteristics

1. Digital 8 Format 90 minutes in Short Play (SP) Mode
135 minutes in Long Play (LP) Mode.
2. Hi 8 Format 150 minutes maximum. Operating Temperature Range -55� C to +70� C.
3. Dimension 172 x 130 x 204.
4. Weights less than 3.3 kg.

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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.

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التعديل الأخير:
رد: الصناعة العسكرية الباكستانية

انظمه تحكم ارتفاع و طيران لطائرات صناعه باكستانيه

ATTITUDE & HEADING REFERENCE SYSTEM

Category : Altitude & Heading Reference System
Manufacturer : GIDS
Detail
LISA
For More Details Please

Click here to view the original image of 720x565px.
LISA.jpg
 
رد: الصناعة العسكرية الباكستانية

انظمه محافظ شاف و فلير لحمايه الطائرات من صواريخ
MOHAFIZ (CHAFF & FLARE DISPENSER SYSTEM)

Category : Infrared Flares & Dispenser System
Manufacturer : GIDS
Detail


MOHAFIZ Counter Measures System is designed and produced for military aircraft and helicopter applications.
Product System Definition
Standard MOHAFIZ Counter Measures System:

1. 1 x Display and control Unit (DCU)
2. 1 x Control processing Unit (CPU)
3. 1 x Fire Control Unit(FCU)
4. 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. 1 x Display Control Unit (CCU)
2. 1 x Control Processing Unit (CPU)
3. 1 x Fire Control Unit (FCU)
4. 1 x Dispensers Unit

System Features

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

Flare Characteristics

1. Jamming Wavelength: 1-5 micron
2. Peak static radiation intensity: >20 KW/Sr
3. Flare rise time: <0.25 sec
4. Flare burn time: >3.5 sec
5. Initial Ejection Velocity: >25 m/sec





Chaff Characteristics

* Frequency range: 2-18 GHz
* RCS: >10 m(sqr)
* Chaff Bloom Time: <500 ms
* Initial Ejection Velocity: 15-25 m/sec
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


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Mohafiz-02.jpg

 
رد: الصناعة العسكرية الباكستانية


Ultra Quick Electronic Impact Fuze

* AB-100 AN
* AB-100 (For Low Drag Bombs).
* AB-105 (For Low & High Drag Bombs).

Electronic Proximity Fuze

* AB-103 (For Low Drag Bombs).
* AB-104 (For Low & High Drag Bombs).
* AB-104 AN (For Low & High Drag Bombs).

Multi-Role Fuze

* AL-788.

Common Features

* Incorporates state-of-the-art electronics, including such advanced features as a microprocessor based controller and a stepper motor to perform mechanical safety functions.
* Functioning is regulated by a microprocessor based controller.
* Designed for impact detonating action (including backup impact function) on all types of targets, including water and soft ground.
* Includes bird strike safety in all fuze types.



FEATURES OF AIR BURST FUZES AB-103 & AB-104


* Optimizes the performance of air-burst bombs.
* The proximity function ensures a 2-12 m above ground level burst of the bomb for all types of targets, approach angles and closing velocities.
* Smoke or dust on the terrain does not interfere with the proximity function and electronic circuitry provides high immunity against enemy jamming.



FEATURES OF GROUND BURST FUZES AB-100 & AB-105


* High performance electronic fuze replacement for M-904 Fuze or equivalent mechanical type fuzes.
* Optimizes the performance of ground-burst bombs.
* Provides instantaneous firing pulse (less than 50 micro seconds) on impact, thus ensuring true surface detonation of the bomb.



SPECIAL FEATURES OF AB-104 & AB-105


* The presence of G-Sensor guarantees that the AB-104/AB-105 will not arm if The retarted tail unit does not open fully.



SPECIFICATIONS

AB-100 AB-103 AB-104 AB-105 AL-788
Operation High Performance Ultra Quick Impact Detonating System High Performance Proximity/Impact Detonating System High Performance Proximity/Impact Detonating System High Performance Ultra Quick Impact Detonating System This Versatile Nose Fuze offers Proximity and Impact Detonation Modes Both in High and Low Drag Configuration
Burst Height - 2 - 12 m Above the surface 2 - 12 m Above the surface - 2 - 12 m Above the surface
Safety
Selectable Arming Time 4-18 Seconds in low drag 2-6 Seconds in high drag mode, 4-30 Seconds in low drag mode
Electronic Module Activation Light
Air Sensor used to ensure that the fuze will not arm if the air speed is less than 220 knots
Carriage Envelope
Speed 0 to 600 knots IAS
Altitude 0 to 40,000 Feet
G-Loading - 2.5 g to +6 g
Roll Rate 165 Degrees / Second
Environment Testing As per MIL-STD-331 and MIL-STD-810
Temperature Range -40o C to +71o C
Power Source Lithium Batteries
Reliability 95 %
Storage Life 8 - 10 Years
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