Imran Khan
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Stun Granades
Category : Stun Granades
Manufacturer : GIDS
Detail
Category : Stun Granades
Manufacturer : GIDS
Detail
PWI | Pakistan Weapons Industry
- Thread starter Imran Khan
- Start date
Imran Khan
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STUN GRENADE
Category : Stun Granades
Manufacturer : GIDS
Detail
A device to produce high intensity illumination and loud bang which temporarily causes disorientation of the other persons.
* It is non lethal and does not contain explosive material.
* No fragments are produced after initiation.
SPECIFICATIONS
Illumination intensity
Sound Intensity
Delay Time
Total weight of the Device
Diameter of the Body
Length of the Body
10,000 ft Candle
120 dbs approx.
1.5 - 2 Seconds
230 g approx.
51.50mm
165.00mm
Category : Stun Granades
Manufacturer : GIDS
Detail
A device to produce high intensity illumination and loud bang which temporarily causes disorientation of the other persons.
* It is non lethal and does not contain explosive material.
* No fragments are produced after initiation.
SPECIFICATIONS
Illumination intensity
Sound Intensity
Delay Time
Total weight of the Device
Diameter of the Body
Length of the Body
10,000 ft Candle
120 dbs approx.
1.5 - 2 Seconds
230 g approx.
51.50mm
165.00mm
Frankenstein
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I would like to thank India, If they were not are adversary, then we would never have gone that far in tech
Imran Khan
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Ballistic helmets
Category : Ballistic Helmets
Manufacturer : GIDS
Detail
Ballistic Helmet
Key Specification / Special Features
* Our PASGT (Personal Armour system Ground Troops) helmet protects against fragments / shrapnel & ballistic threats.
* Manufactured using Aramid, high strength low weight textile fiber, and resin having high ballistic resistance.
* Comfortable wearing with ideal mass distribution over head.
* Used by military, special forces and police.
Colors
Easy to camouflage / conceal as it is available in army green, desert tan, black or in any other color as per requirement. Yarn of chain strap dyed in non fading color, resistant to perspiration, water & heat.
Design Configuration
* Compatible with goggles, binoculars & wireless communication devices
* Adjustable chin strap.
* Allows good air circulation.
Manufacturing & Testing Facilities
We have the facility to impregnate mold & test the Composite / Aramid material as well as the facility to test the ballistic helmet according to international standards.
Protection Levels
Ballistic resistant
Ballistic Penetration Resistance is according to NIJ-STD-0101.01 for following ammunition & weapons.
* Ammunition Cal. 9mmx12g MK 20AMD
* Weapon SMG,MP5A2A3
* Nominal Bullet Mass 7.45 gm
* Muzzle Energy 626J
* Trauma 20mm
Resistance against heat & water
Inner suspension system provides heat resistance from hot environment. Ballistic performance not effected even after long exposure of water.
Price
We offer highly competitive prices of all models.
Available Sizes
We offer varying weights & sizes to suit your needs. It's perfect fit and comfort makes it possible to be worn for a longer period of time.
helmet
Category : Ballistic Helmets
Manufacturer : GIDS
Detail
Ballistic Helmet
Key Specification / Special Features
* Our PASGT (Personal Armour system Ground Troops) helmet protects against fragments / shrapnel & ballistic threats.
* Manufactured using Aramid, high strength low weight textile fiber, and resin having high ballistic resistance.
* Comfortable wearing with ideal mass distribution over head.
* Used by military, special forces and police.
Colors
Easy to camouflage / conceal as it is available in army green, desert tan, black or in any other color as per requirement. Yarn of chain strap dyed in non fading color, resistant to perspiration, water & heat.
Design Configuration
* Compatible with goggles, binoculars & wireless communication devices
* Adjustable chin strap.
* Allows good air circulation.
Manufacturing & Testing Facilities
We have the facility to impregnate mold & test the Composite / Aramid material as well as the facility to test the ballistic helmet according to international standards.
Protection Levels
Ballistic resistant
Ballistic Penetration Resistance is according to NIJ-STD-0101.01 for following ammunition & weapons.
* Ammunition Cal. 9mmx12g MK 20AMD
* Weapon SMG,MP5A2A3
* Nominal Bullet Mass 7.45 gm
* Muzzle Energy 626J
* Trauma 20mm
Resistance against heat & water
Inner suspension system provides heat resistance from hot environment. Ballistic performance not effected even after long exposure of water.
Price
We offer highly competitive prices of all models.
Available Sizes
We offer varying weights & sizes to suit your needs. It's perfect fit and comfort makes it possible to be worn for a longer period of time.
helmet
Imran Khan
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GENERAL PURPOSE STEEL BOMBS
DESCRIPTION
* Effective against all kind of targets.
* 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 filling can be used for training purpose.
* Can be used in the following configurations:-
o Low drag configuration: when installed with Conical Fin Assembly.
o High drag configuration: when installed with Retarded Tail Unit.
* Can be fitted with the following types of fuzes:-
o Mechanical Nose fuze M-904 or equivalent.
o Mechanical Tail fuze M-905 or equivalent.
NATO APPLICATIONS
* Can be carried on NATO standard suspension systems.
* Can be fitted with the following types of Electronic fuzes:-
o Ultra Quick Electronic Impact Nose Fuzes AB-100 ( in low drag configuration) and AB-105 (in low or high drag configuration).
o Electronic Proximity Nose Fuzes AB-103 (in low drag configuration) and AB-104 (in low or high drag configuration).
o Electronic Long Delay Fuze AB-112.
o Electrically Timed Fuzes FMU-81/B, FMU-139 A/B.
o Electronic (Tail) Fuze FMU-54 A/B.
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.
* Can be fitted with the following types of Electronic fuzes.
o Ultra Quick Electronic Impact nose Fuzes AB-100AN (in low drag configuration) and AB-105AN (In low or high drag configuration).
o Electronic Proximity Nose Fuzes AB-103AN (in low drag configuration) and AB-104AN (in low or high drag configuration). Electronic Long Delay Fuze AB-112AN
o Electrically Timed Fuzes FMU-81/B, FMU-139 A/B
o Electronic (Tail) Fuze FMU-54 A/B
SPECIFICATIONS
General Purpose Steel Bomb(125 Kg)
General Purpose Steel Bomb(250 Kg)
General Purpose Steel Bomb(500 Kg)
General Purpose Steel Bomb(1000 Kg)
GP Steel NATO GP Steel WARSAW GP Steel NATO GP Steel WARSAW GP Steel NATO GP Steel WARSAW GP Steel NATO GP Steel WARSAW
Length 1,072 mm - 1,084.5 mm 1,531 mm - 1,547 mm 1,832 mm - 1,850 mm 2,466 mm - 2,482 mm
Diameter Ø 228.60 mm Ø 273.10 mm Ø 356.6 mm Ø 457.00 mm
Net Explosive Content 45 kg 87 kg 200 kg 430 kg
Type of Explosive Composition 'B' (Typical) Composition 'B' (Typical) Composition 'B' (Typical) Composition 'B' (Typical)
Charge Weight Ratio 36% to 40% 40%
Aircraft Interface 355.60 mm(14 inch) apart suspension lugs 250.00 mm apart suspension lugs 355.60 mm(14 inch) apart suspension lugs 250.00 mm apart suspension lugs 355.60 mm(14 inch) apart suspension lugs 250.00 mm apart suspension lugs 762.00 mm(30 inch) apart suspension lugs 480.00 mm apart suspension lugs
Integral E.F.I. Cable - Yes - Yes - Yes - Yes
Service Life 10 years (Subject to AERO Defined Storage Standards)
DESCRIPTION
* Effective against all kind of targets.
* 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 filling can be used for training purpose.
* Can be used in the following configurations:-
o Low drag configuration: when installed with Conical Fin Assembly.
o High drag configuration: when installed with Retarded Tail Unit.
* Can be fitted with the following types of fuzes:-
o Mechanical Nose fuze M-904 or equivalent.
o Mechanical Tail fuze M-905 or equivalent.
NATO APPLICATIONS
* Can be carried on NATO standard suspension systems.
* Can be fitted with the following types of Electronic fuzes:-
o Ultra Quick Electronic Impact Nose Fuzes AB-100 ( in low drag configuration) and AB-105 (in low or high drag configuration).
o Electronic Proximity Nose Fuzes AB-103 (in low drag configuration) and AB-104 (in low or high drag configuration).
o Electronic Long Delay Fuze AB-112.
o Electrically Timed Fuzes FMU-81/B, FMU-139 A/B.
o Electronic (Tail) Fuze FMU-54 A/B.
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.
* Can be fitted with the following types of Electronic fuzes.
o Ultra Quick Electronic Impact nose Fuzes AB-100AN (in low drag configuration) and AB-105AN (In low or high drag configuration).
o Electronic Proximity Nose Fuzes AB-103AN (in low drag configuration) and AB-104AN (in low or high drag configuration). Electronic Long Delay Fuze AB-112AN
o Electrically Timed Fuzes FMU-81/B, FMU-139 A/B
o Electronic (Tail) Fuze FMU-54 A/B
SPECIFICATIONS
General Purpose Steel Bomb(125 Kg)
General Purpose Steel Bomb(250 Kg)
General Purpose Steel Bomb(500 Kg)
General Purpose Steel Bomb(1000 Kg)
GP Steel NATO GP Steel WARSAW GP Steel NATO GP Steel WARSAW GP Steel NATO GP Steel WARSAW GP Steel NATO GP Steel WARSAW
Length 1,072 mm - 1,084.5 mm 1,531 mm - 1,547 mm 1,832 mm - 1,850 mm 2,466 mm - 2,482 mm
Diameter Ø 228.60 mm Ø 273.10 mm Ø 356.6 mm Ø 457.00 mm
Net Explosive Content 45 kg 87 kg 200 kg 430 kg
Type of Explosive Composition 'B' (Typical) Composition 'B' (Typical) Composition 'B' (Typical) Composition 'B' (Typical)
Charge Weight Ratio 36% to 40% 40%
Aircraft Interface 355.60 mm(14 inch) apart suspension lugs 250.00 mm apart suspension lugs 355.60 mm(14 inch) apart suspension lugs 250.00 mm apart suspension lugs 355.60 mm(14 inch) apart suspension lugs 250.00 mm apart suspension lugs 762.00 mm(30 inch) apart suspension lugs 480.00 mm apart suspension lugs
Integral E.F.I. Cable - Yes - Yes - Yes - Yes
Service Life 10 years (Subject to AERO Defined Storage Standards)
Imran Khan
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PRE-FRAGMENTED BOMBS
DESCRIPTION
* New concept in optimizing the effectiveness of conventional bombs.
* Outer casing manufactured from composite fiber.
* 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.
* Filled with compo 'B' explosive
* Inert filling can be used for training purpose
* High Length-to-Diameter Ratio for low drag design
* Can be used in the following configuration:-
o Low drag configuration : when installed with Conical Fin Assembly.
o High drag configuration : when installed with Retarded Tail Unit.
NATO APPLICATIONS
* Can be carried on NATO standard suspension system.
* Can be fitted with the following types of fuzes:-
o Ultra Quick Electronic Impact Nose Fuzes AB-100 (in low drag configuration ) and AB-105(in low or high drag configuration)
o 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.
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.
* Can be fitted with the following types of fuzes:-
o Ultra Quick Electronic Impact Nose Fuzes AB-100AN (in low drag configuration) and AB-105AN (in low or high drag configuration)
o Electronic Proximity Nose Fuze AB-103AN (in low drag configuration) and AB-104AN (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.
SPECIFICATIONS
Pre-Fragmented Bomb (125 Kg)
Pre-Fragmented Bomb (250 Kg)
Pre-Fragmented Bomb (500 Kg)
Pre-Fragmented Bomb (1000 Kg)
PF NATO PF WARSAW PF NATO PF WARSAW PF NATO PF WARSAW PF NATO PF WARSAW
Length 1,072 mm - 1,084.5 mm 1,531 mm - 1,547 mm 1,832 mm - 1,850 mm 2, 466 mm - 2,482 mm
Diameter Ø 228.60 mm Ø 273.10 mm Ø 355.6 mm Ø 4,57.00 mm
Net Explosive Content 24 - 27 kg 48 - 51 kg 71- 79 kg 198 - 208 kg
Type of Explosive Composition 'B' (Typical) Composition 'B' (Typical) Composition 'B' (Typical) Composition 'B' (Typical)
Charge Weight Ratio 18% to 20% 18% to 20% 18% to 20% 18% to 20%
Aircraft Interface 355.60 mm(14 inch) apart suspension lugs 250.00 mm apart suspension lugs 355.60 mm(14 inch) apart suspension lugs 250.00 mm apart suspension lugs 355.60 mm(14 inch) apart suspension lugs 250.00 mm apart suspension lugs 762.00 mm(30 inch) apart suspension lugs 480.00 mm(30 inch) apart suspension lugs
Integral E.F.I. Cable - Yes - Yes - Yes - Yes
Typical Application Antipersonal Antipersonal and thin skin vehicles. Thin skin and light amour. Demolition
No. Of Steel Balls 20,000 11,900 10,780 4,900
Diameter of Steel Balls Ø 8.70 mm Ø 15.90 mm Ø 15.90 mm Ø 25.00 mm
Weight per 1000 Balls 2.65 kgs 8.42 kgs 18 kgs 67.36 kgs
Service Life 10 years (Subject to AERO Defined Storage Standards)
DESCRIPTION
* New concept in optimizing the effectiveness of conventional bombs.
* Outer casing manufactured from composite fiber.
* 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.
* Filled with compo 'B' explosive
* Inert filling can be used for training purpose
* High Length-to-Diameter Ratio for low drag design
* Can be used in the following configuration:-
o Low drag configuration : when installed with Conical Fin Assembly.
o High drag configuration : when installed with Retarded Tail Unit.
NATO APPLICATIONS
* Can be carried on NATO standard suspension system.
* Can be fitted with the following types of fuzes:-
o Ultra Quick Electronic Impact Nose Fuzes AB-100 (in low drag configuration ) and AB-105(in low or high drag configuration)
o 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.
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.
* Can be fitted with the following types of fuzes:-
o Ultra Quick Electronic Impact Nose Fuzes AB-100AN (in low drag configuration) and AB-105AN (in low or high drag configuration)
o Electronic Proximity Nose Fuze AB-103AN (in low drag configuration) and AB-104AN (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.
SPECIFICATIONS
Pre-Fragmented Bomb (125 Kg)
Pre-Fragmented Bomb (250 Kg)
Pre-Fragmented Bomb (500 Kg)
Pre-Fragmented Bomb (1000 Kg)
PF NATO PF WARSAW PF NATO PF WARSAW PF NATO PF WARSAW PF NATO PF WARSAW
Length 1,072 mm - 1,084.5 mm 1,531 mm - 1,547 mm 1,832 mm - 1,850 mm 2, 466 mm - 2,482 mm
Diameter Ø 228.60 mm Ø 273.10 mm Ø 355.6 mm Ø 4,57.00 mm
Net Explosive Content 24 - 27 kg 48 - 51 kg 71- 79 kg 198 - 208 kg
Type of Explosive Composition 'B' (Typical) Composition 'B' (Typical) Composition 'B' (Typical) Composition 'B' (Typical)
Charge Weight Ratio 18% to 20% 18% to 20% 18% to 20% 18% to 20%
Aircraft Interface 355.60 mm(14 inch) apart suspension lugs 250.00 mm apart suspension lugs 355.60 mm(14 inch) apart suspension lugs 250.00 mm apart suspension lugs 355.60 mm(14 inch) apart suspension lugs 250.00 mm apart suspension lugs 762.00 mm(30 inch) apart suspension lugs 480.00 mm(30 inch) apart suspension lugs
Integral E.F.I. Cable - Yes - Yes - Yes - Yes
Typical Application Antipersonal Antipersonal and thin skin vehicles. Thin skin and light amour. Demolition
No. Of Steel Balls 20,000 11,900 10,780 4,900
Diameter of Steel Balls Ø 8.70 mm Ø 15.90 mm Ø 15.90 mm Ø 25.00 mm
Weight per 1000 Balls 2.65 kgs 8.42 kgs 18 kgs 67.36 kgs
Service Life 10 years (Subject to AERO Defined Storage Standards)
Imran Khan
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INCENDIARY PRE-FRAGMENTED BOMBS
DESCRIPTION
* New concept in optimizing the effectiveness of conventional bombs.
* A combination of steel balls and especially developed incendiary metal alloy is used to effectively create incendiary effect.
* Outer casing manufactured from composite fiber.
* 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.
* Filled with compo 'B' explosive
* Inert filling can be used for training purpose.
* High Length-To-Diameter Ratio for low drag design.
* Can be used in the following configuration:-
o Low drag configuration : when installed with Conical Fin Assembly.
o High drag configuration : when installed with Retarded Tail Unit.
NATO APPLICATIONS
* Can be carried on NATO standard suspension system.
* Can be fitted with the following types of fuzes:-
o Ultra Quick Electronic Impact Nose Fuzes AB-100 (in low drag configuration ) and AB-105 (in low or high drag configuration)
o Electronic Proximity Nose 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.
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.
* Can be fitted with the following types of fuzes:-
o Ultra Quick Electronic Impact Nose Fuzes AB-100AN (in low drag configuration) and AB-105AN (in low or high drag configuration).
o Electronic Proximity Nose Fuze AB - 103AN (in low drag configuration) and AB-10AN (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
SPECIFICATIONS
Incendiary Pre-Fragmented Bomb (125 Kg)
Incendiary Pre-Fragmented Bomb (250 Kg)
Incendiary Pre-Fragmented Bomb (500 Kg)
PFI NATO PFI WARSAW PFI NATO PFI WARSAW PFI NATO PFI WARSAW
Length 1,072 mm - 1,084.5 mm 1,531 mm - 1,547 mm 1,832 mm - 1,850 mm
Diameter Ø 228.60 mm Ø 273.10 mm Ø 355.6 mm
Net Explosive Content 24 - 27 kg 48 - 51 kg 71- 79 kg
Type of Explosive Composition 'B' (Typical) Composition 'B' (Typical) Composition 'B' (Typical)
Charge Weight Ratio 18% to 20% 18% to 20% 18% to 20%
Aircraft Interface 355.60 mm(14 inch) apart suspension lugs 250.00 mm apart suspension lugs 355.60 mm(14 inch) apart suspension lugs 250.00 mm apart suspension lugs 355.60 mm(14 inch) apart suspension lugs 250.00 mm apart suspension lugs
Integral E.F.I. Cable - Yes - Yes - Yes
Typical Application Incendiary- Heat stroke,Pulmonary effects, Oxygen starvation, Severe burns. Incendiary effect on POL and combustible materials. Pre-Fragmented- Anti-personnel and soft skin Incendiary- Heat stroke, Pulmonary effects, Oxygen starvation, Severe burns. Incendiary effect on POL and combustible materials. Pre-Fragmented- Anti-personnel and soft skin Incendiary- Heat stroke, Pulmonary effects, Oxygen starvation, Severe burns. Incendiary effect on POL and combustible materials. Pre-Fragmented- Anti-personnel and soft skin
No. Of Incendiary pieces 380 300 1040
Size of Incendiary pieces Ø 15x20x26 mm Ø 20x30x50 mm Ø 22 mm
Incendiary coverage-radius from point of detonation 400 m - 500 m 400 m - 500 m 500 m - 600 m
No. Of Steel Balls 15, 000 9,600 8,670
Diameter of Steel Balls Ø 8.7 mm Ø 8.70 mm or 16 mm To client requirement
Weight per 1000 Balls 2.65 kg 2.65 kg or 18 kg 18 kg
Service Life 10 years (Subject to AERO Defined Storage Standards)
DESCRIPTION
* New concept in optimizing the effectiveness of conventional bombs.
* A combination of steel balls and especially developed incendiary metal alloy is used to effectively create incendiary effect.
* Outer casing manufactured from composite fiber.
* 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.
* Filled with compo 'B' explosive
* Inert filling can be used for training purpose.
* High Length-To-Diameter Ratio for low drag design.
* Can be used in the following configuration:-
o Low drag configuration : when installed with Conical Fin Assembly.
o High drag configuration : when installed with Retarded Tail Unit.
NATO APPLICATIONS
* Can be carried on NATO standard suspension system.
* Can be fitted with the following types of fuzes:-
o Ultra Quick Electronic Impact Nose Fuzes AB-100 (in low drag configuration ) and AB-105 (in low or high drag configuration)
o Electronic Proximity Nose 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.
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.
* Can be fitted with the following types of fuzes:-
o Ultra Quick Electronic Impact Nose Fuzes AB-100AN (in low drag configuration) and AB-105AN (in low or high drag configuration).
o Electronic Proximity Nose Fuze AB - 103AN (in low drag configuration) and AB-10AN (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
SPECIFICATIONS
Incendiary Pre-Fragmented Bomb (125 Kg)
Incendiary Pre-Fragmented Bomb (250 Kg)
Incendiary Pre-Fragmented Bomb (500 Kg)
PFI NATO PFI WARSAW PFI NATO PFI WARSAW PFI NATO PFI WARSAW
Length 1,072 mm - 1,084.5 mm 1,531 mm - 1,547 mm 1,832 mm - 1,850 mm
Diameter Ø 228.60 mm Ø 273.10 mm Ø 355.6 mm
Net Explosive Content 24 - 27 kg 48 - 51 kg 71- 79 kg
Type of Explosive Composition 'B' (Typical) Composition 'B' (Typical) Composition 'B' (Typical)
Charge Weight Ratio 18% to 20% 18% to 20% 18% to 20%
Aircraft Interface 355.60 mm(14 inch) apart suspension lugs 250.00 mm apart suspension lugs 355.60 mm(14 inch) apart suspension lugs 250.00 mm apart suspension lugs 355.60 mm(14 inch) apart suspension lugs 250.00 mm apart suspension lugs
Integral E.F.I. Cable - Yes - Yes - Yes
Typical Application Incendiary- Heat stroke,Pulmonary effects, Oxygen starvation, Severe burns. Incendiary effect on POL and combustible materials. Pre-Fragmented- Anti-personnel and soft skin Incendiary- Heat stroke, Pulmonary effects, Oxygen starvation, Severe burns. Incendiary effect on POL and combustible materials. Pre-Fragmented- Anti-personnel and soft skin Incendiary- Heat stroke, Pulmonary effects, Oxygen starvation, Severe burns. Incendiary effect on POL and combustible materials. Pre-Fragmented- Anti-personnel and soft skin
No. Of Incendiary pieces 380 300 1040
Size of Incendiary pieces Ø 15x20x26 mm Ø 20x30x50 mm Ø 22 mm
Incendiary coverage-radius from point of detonation 400 m - 500 m 400 m - 500 m 500 m - 600 m
No. Of Steel Balls 15, 000 9,600 8,670
Diameter of Steel Balls Ø 8.7 mm Ø 8.70 mm or 16 mm To client requirement
Weight per 1000 Balls 2.65 kg 2.65 kg or 18 kg 18 kg
Service Life 10 years (Subject to AERO Defined Storage Standards)
Imran Khan
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- Oct 18, 2007
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CEM (COMBINED EFFECT MUNITION)
INTRODUCTION
Combined Effect Munition (CEM) is conventional cluster bomb with two kill mechanism:
* Anti-Personnel: Mild steel bomblet body having a warhead containing steel balls for fragmentation.
* Anti-Armor: Copper cone based shaped charge for armor penetration.
Combined Effect Munitions (CEM) consists of MK-7 Dispenser containing 247 Combined Effect Bomblets (CEBs).
The dual kill capability of CEM allows multi-dimensional damage to variety of targets.
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 Effect Bomblets (CEB) are dispersed in a stabilized nose down from over the pre-planed coverage area. Ram air causes the vane of S&A to rotate at high RPM, which result in the 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+10lbs
* Diameter: 13.20 inches
* Cross-section: 137 in2
* Fin Span (closed): 17.2 in2
* Lug Spacing: 14 inches
* Fuze Type: Electronic time based, nose mounted
FUZE SAFETY FEATURES
* Air Sensor to check 220 knots
* Electro-mechanical system for explosive train alignment
* No. of Bomblets: 247
* Bomblet Warhead: Anti Personnel, Anti Armor
PERFORMANCES SPECIFICATION
* Launch Speeds: 400-600 KTAS
* Launch Altitude: 100 m (level)
* Angle of Attack: 0 to 60 Degrees
* Operational Temperature Range: -40o C to +71o C
* Environmental Qualification: As per MIL-STD-331 and MIL-STD-810F
* Carriage Qualification: Same as MK-20
* Shelf Life: 10 Years
* Targets: Personnel, Armored Vehicles
INTRODUCTION
Combined Effect Munition (CEM) is conventional cluster bomb with two kill mechanism:
* Anti-Personnel: Mild steel bomblet body having a warhead containing steel balls for fragmentation.
* Anti-Armor: Copper cone based shaped charge for armor penetration.
Combined Effect Munitions (CEM) consists of MK-7 Dispenser containing 247 Combined Effect Bomblets (CEBs).
The dual kill capability of CEM allows multi-dimensional damage to variety of targets.
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 Effect Bomblets (CEB) are dispersed in a stabilized nose down from over the pre-planed coverage area. Ram air causes the vane of S&A to rotate at high RPM, which result in the 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+10lbs
* Diameter: 13.20 inches
* Cross-section: 137 in2
* Fin Span (closed): 17.2 in2
* Lug Spacing: 14 inches
* Fuze Type: Electronic time based, nose mounted
FUZE SAFETY FEATURES
* Air Sensor to check 220 knots
* Electro-mechanical system for explosive train alignment
* No. of Bomblets: 247
* Bomblet Warhead: Anti Personnel, Anti Armor
PERFORMANCES SPECIFICATION
* Launch Speeds: 400-600 KTAS
* Launch Altitude: 100 m (level)
* Angle of Attack: 0 to 60 Degrees
* Operational Temperature Range: -40o C to +71o C
* Environmental Qualification: As per MIL-STD-331 and MIL-STD-810F
* Carriage Qualification: Same as MK-20
* Shelf Life: 10 Years
* Targets: Personnel, Armored Vehicles
Imran Khan
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CONICAL TAIL UNITS
DESCRIPTION
* Stabilizes the flight of the bomb.
* Creates a low drag configuration for the bomb.
* Consists of an elongated cone assembled with four fins.
* Can be fitted with General Purpose Steel And Pre-fragmented Bombs.
SPECIFICATIONS
* Length: 26.12 inches
* Gross Weight: 9.55 kg
* Diameter: 8.76 inches
RETARDED TAIL UNIT
DESCRIPTION
* Especially designed to provide adequate safe distance between the bomb and the delivery aircraft during low level attack.
* Creates a low drag configuration for the bomb when in closed position and a high drag configuration when in open position.
* Consists of a shock absorbing tube and four extendable drag fins.
* After delivery from aircraft, the extended fins decelerate the bomb.
* Can be fitted with General Purpose Steel and Pre-fragmented Bombs.
SPECIFICATIONS
* Length: 31.70 inches
* Gross Weight: 28.18 kg
* Diameter: 15 inches
DESCRIPTION
* Stabilizes the flight of the bomb.
* Creates a low drag configuration for the bomb.
* Consists of an elongated cone assembled with four fins.
* Can be fitted with General Purpose Steel And Pre-fragmented Bombs.
SPECIFICATIONS
* Length: 26.12 inches
* Gross Weight: 9.55 kg
* Diameter: 8.76 inches
RETARDED TAIL UNIT
DESCRIPTION
* Especially designed to provide adequate safe distance between the bomb and the delivery aircraft during low level attack.
* Creates a low drag configuration for the bomb when in closed position and a high drag configuration when in open position.
* Consists of a shock absorbing tube and four extendable drag fins.
* After delivery from aircraft, the extended fins decelerate the bomb.
* Can be fitted with General Purpose Steel and Pre-fragmented Bombs.
SPECIFICATIONS
* Length: 31.70 inches
* Gross Weight: 28.18 kg
* Diameter: 15 inches
Imran Khan
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RPB-1 (Runway Penetration Bomb-1)
DESCRIPTION
* Runway penetration bomb is used to neutralize concrete targets like runways, bunkers etc.
* The effect of destruction is obtained by high speed impact, penetration and then upheaval of hard targets by exploding the warhead with no risk to the delivering aircraft.
* The bomb can be released at high speed and low altitude to avoid enemy defenses.
* Upon delivery, the bomb decelerates to a very low speed to obtain the penetration angle and to increase the safety distance between the bomb and the releasing aircraft. Subsequently the firing of the rocket motor accelerates the bomb to a very high speed for penetration into the hard target.
* Release envelope
o 450 < IAS < 600 knots
o Altitude: ≥ 200 feet
* Consists of four main sub-assemblies:-
o The Warhead: located at the front and weight approximately 105 kg
o The Sequence Assembly:located immediately behind the warhead and controls the sequence of operations.
o The Parachute Section: attached to the rear skirt of the booster by a jettisonable clamp ring and contains two drag chutes (deceleration and main).
o The Rocket Motor: double base propellant, burns for 0.45 seconds and provides a Thrust of 10,000 DaN
* Can be carried on NATO standard suspension systems
OPERATION
Stored in a special sealed container, allowing installation on the aircraft directly from the container without any pre-installation assembly or adjustment.
Retarded Phase:
* Ejection of drag chute.
* Deployment of the first drag chute.
* Ejection and deployment of main chute.
* Measurement of the acceleration / time conditions.
Acceleration Phase:
* Ejection of the main chute and ignition of the rocket motor.
* Accelerates to 250 m/s in 0.45 seconds.
* Impact and explosion after penetration.
In case of emergency jettisoning, bomb drops completely inert.
DIMENSIONS
* Overall Length: 2491 mm
* Length excluding the Front Fairing: 2414 mm
* Maximum Body Diameter: 223 mm
* Maximum Span: 430 mm
* Approximate Overall Propelled Weight: 165 kg
* Approximate Launch Weight: 200 kg
SAFETY
* No electrical ignition.
* Drag chutes are not locked during captive flight.
* Rocket motor does not fire if main chute is not deployed for sufficient time.
* The warhead fuze pyrotechnic train stays out of line before Firing of rocket motor.
DESCRIPTION
* Runway penetration bomb is used to neutralize concrete targets like runways, bunkers etc.
* The effect of destruction is obtained by high speed impact, penetration and then upheaval of hard targets by exploding the warhead with no risk to the delivering aircraft.
* The bomb can be released at high speed and low altitude to avoid enemy defenses.
* Upon delivery, the bomb decelerates to a very low speed to obtain the penetration angle and to increase the safety distance between the bomb and the releasing aircraft. Subsequently the firing of the rocket motor accelerates the bomb to a very high speed for penetration into the hard target.
* Release envelope
o 450 < IAS < 600 knots
o Altitude: ≥ 200 feet
* Consists of four main sub-assemblies:-
o The Warhead: located at the front and weight approximately 105 kg
o The Sequence Assembly:located immediately behind the warhead and controls the sequence of operations.
o The Parachute Section: attached to the rear skirt of the booster by a jettisonable clamp ring and contains two drag chutes (deceleration and main).
o The Rocket Motor: double base propellant, burns for 0.45 seconds and provides a Thrust of 10,000 DaN
* Can be carried on NATO standard suspension systems
OPERATION
Stored in a special sealed container, allowing installation on the aircraft directly from the container without any pre-installation assembly or adjustment.
Retarded Phase:
* Ejection of drag chute.
* Deployment of the first drag chute.
* Ejection and deployment of main chute.
* Measurement of the acceleration / time conditions.
Acceleration Phase:
* Ejection of the main chute and ignition of the rocket motor.
* Accelerates to 250 m/s in 0.45 seconds.
* Impact and explosion after penetration.
In case of emergency jettisoning, bomb drops completely inert.
DIMENSIONS
* Overall Length: 2491 mm
* Length excluding the Front Fairing: 2414 mm
* Maximum Body Diameter: 223 mm
* Maximum Span: 430 mm
* Approximate Overall Propelled Weight: 165 kg
* Approximate Launch Weight: 200 kg
SAFETY
* No electrical ignition.
* Drag chutes are not locked during captive flight.
* Rocket motor does not fire if main chute is not deployed for sufficient time.
* The warhead fuze pyrotechnic train stays out of line before Firing of rocket motor.
Last Hope
SENIOR MEMBER
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If we had 'The best thread' option, I am sure this would win.
This page is espicially better than the first one, and it is total astonishment to see the great stuff we can make and also to know that we have capability to make stuff greater than this.
This page is espicially better than the first one, and it is total astonishment to see the great stuff we can make and also to know that we have capability to make stuff greater than this.
Imran Khan
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- Oct 18, 2007
- Messages
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mamooooo abhi to 2 companies bhi compleate nhi hoi pakistan ke 23 companies hai defence product making ki heheeheh
Imran Khan
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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
* 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
Imran Khan
PDF VETERAN
- Joined
- Oct 18, 2007
- Messages
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Electronic Proximity Fuze
* AB-100 AN (For Low Drag Bombs).
* AB-104 (For Low & High Drag Bombs).
* AB-104 AN (For Low & High Drag Bombs).
Common Features
* Optimizes the performance of air-burst bombs.
* Incorporates state-of-the-art electronics, including such advanced features as microprocessor based controller and a stepper motor to perform mechanical safety functions.
* Designed for impact detonating action (including backup impact functions) on all types of targets, including water and soft ground.
* Smoke or dust on the terrain does not interfere with the proximity function, and electronic circuitry provides high immunity against enemy jamming.
* Includes E.F.I capability for interface to Russian aircraft pylons.
SPECIAL FEATURES OF AB-104 AN
* The presence of G-Sensor guarantees that the fuze will not arm if the Retarded tail unit does not open fully.
* 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.
SPECIFICATIONS
AB-104 AN AB-100 AN
Operation High / Low Drag Proximity Fuze with backup Impact Detonating High Performance Ultra Quick Impact Detonating System
Burst Height 2 - 12 m above the Surface -
Safety
Selectable Arming Time 2-6 Seconds in high drag mode, 4-30 Seconds in low drag mode 4 - 18 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
E.F.I used to ensure safe separation from the pylon prior to fuze commencing the arming cycle
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
* AB-100 AN (For Low Drag Bombs).
* AB-104 (For Low & High Drag Bombs).
* AB-104 AN (For Low & High Drag Bombs).
Common Features
* Optimizes the performance of air-burst bombs.
* Incorporates state-of-the-art electronics, including such advanced features as microprocessor based controller and a stepper motor to perform mechanical safety functions.
* Designed for impact detonating action (including backup impact functions) on all types of targets, including water and soft ground.
* Smoke or dust on the terrain does not interfere with the proximity function, and electronic circuitry provides high immunity against enemy jamming.
* Includes E.F.I capability for interface to Russian aircraft pylons.
SPECIAL FEATURES OF AB-104 AN
* The presence of G-Sensor guarantees that the fuze will not arm if the Retarded tail unit does not open fully.
* 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.
SPECIFICATIONS
AB-104 AN AB-100 AN
Operation High / Low Drag Proximity Fuze with backup Impact Detonating High Performance Ultra Quick Impact Detonating System
Burst Height 2 - 12 m above the Surface -
Safety
Selectable Arming Time 2-6 Seconds in high drag mode, 4-30 Seconds in low drag mode 4 - 18 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
E.F.I used to ensure safe separation from the pylon prior to fuze commencing the arming cycle
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
