chami t

Junior member
  • Nov 22, 2008
    654
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    kandy
    i got some details [FONT=verdana, geneva, helvetica]of [/FONT][FONT=verdana, geneva, helvetica]United States Military Weapons this is it what u think
    :confused::confused::confused::confused::confused::confused::confused::confused::confused::confused::confused::confused::confused::confused::confused::confused::confused:
    [/FONT][FONT=verdana, geneva, helvetica]:yes::yes::yes::yes::yes::yes::yes::yes::yes::yes::yes::yes::yes::yes::yes::yes::yes:[/FONT][FONT=verdana, geneva, helvetica]
    [/FONT][FONT=verdana, geneva, helvetica][/FONT]
     

    Osama@EK

    Member
    Dec 25, 2008
    144
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    Its a Secret
    chami t said:
    i got some details [FONT=verdana, geneva, helvetica]of [/FONT][FONT=verdana, geneva, helvetica]United States Military Weapons this is it what u think
    :confused::confused::confused::confused::confused::confused::confused::confused::confused::confused::confused::confused::confused::confused::confused::confused::confused:
    [/FONT][FONT=verdana, geneva, helvetica]:yes::yes::yes::yes::yes::yes::yes::yes::yes::yes::yes::yes::yes::yes::yes::yes::yes:[/FONT][FONT=verdana, geneva, helvetica][/FONT]
    Where is the weapons...........:growl::growl::growl::growl:
     

    chami t

    Junior member
  • Nov 22, 2008
    654
    10
    18
    kandy
    Small Arms
    m16a2rifle.gif


    [FONT=verdana, geneva, helvetica]M16A2 Rifle. The M16A2 is the standard issue rifle. It's carried by pretty much every soldier in a combat zone. Most people simply call it the M-16. The M-16 has been around in one version or another since the Vietnam war (the first version, the M16A1 entered Army service in 1964). It's longevity is creditable to its usefulness as a general assault weapon. It's quite simply one of the finest military rifles ever made (although advocates of the M-4 Carbine may argue with me). The rifle is lightweight, simple to operate, and puts out a lot of lead.[/FONT] [FONT=verdana, geneva, helvetica]The M16A2 5.56mm rifle is a lightweight, air-cooled, gas-operated, magazine-fed, shoulder or hip-fired weapon designed for either automatic fire (3-round bursts) or semiautomatic fire (single shot) through the use of a selector lever. The weapon has a fully adjustable rear sight. The bottom of the trigger guard opens to provide access to the trigger while wearing winter mittens. The upper receiver/barrel assembly has a fully adjustable rear sight and a compensator which helps keep the muzzle down during firing. The steel bolt group and barrel extension are designed with locking lugs which lock the bolt group to the barrel extension allowing the rifle to have a lightweight aluminum receiver. [/FONT]
    [FONT=verdana, geneva, helvetica]Primary function: Infantry weapon
    Manufacturer: Colt Manufacturing and Fabrique Nationale Manufacturing Inc.
    Length: 39.63 inches (100.66 centimeters)
    Weight, with 30 round magazine: 8.79 pounds (3.99 kilograms)
    Bore diameter: 5.56mm (.233 inches)
    Maximum effective range:
    Area target: 2,624.8 feet (800 meters)
    Point target: 1,804.5 feet (550 meters)
    Muzzle velocity: 2,800 feet (853 meters) per second
    Rate of fire:
    Cyclic: 800 rounds per minute
    Sustained: 12-15 rounds per minute
    Semiautomatic: 45 rounds per minute
    Burst: 90 rounds per minute
    Magazine capacity: 30 rounds
    Unit Replacement Cost: $586
    [/FONT]
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    [FONT=Verdana, Arial, Helvetica, sans-serif]M-4 Carbine[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The M-4 combat assault rifle first entered Army service in 1997. The rifle is the standard weapon used by some Army units such as the 82nd Airborne Division and special operations units, such as Army Rangers. [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]
    m-4-carbine.gif
    With a shortened barrel and collapsible stock, the M-4 is ideal for close quarter marksmanship where light weight and quick action are required. Firing a standard 5.56 millimeter round, the weapon weighs a mere 5.6 lbs. (empty). A revised rear sight allows for better control of the weapon out to the maximum range of the ammunition used. With the PAQ-4 (Infrared Sight) mounted on the forward rail system, the M-4 can be fitted for increased firepower.
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The M-4 Carbine can also be fitted with the M-203 40mm grenade launcher. The M-203 is a lightweight, compact, breech loading, pump action, single shot launcher. The launcher consists of a hand guard and sight assembly with an adjustable metallic folding, short-range blade sight assembly, and an aluminum receiver assembly which houses the barrel latch, barrel stop and firing mechanism. The launcher is capable of firing a variety of low velocity 40mm ammunition. The launcher also has a quadrant sight that may be attached to the M-4 carrying handle and is used when precision is required out to the maximum effective range of the weapon. The M-4 in this photograph also has an M-68 close-quarters battle sight mounted on the rear rail and a PAQ-4 infra-red sight on the forward rail. [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Type: Compact assault rifle
    Entered Army Service: 1997
    Specifications:
    Caliber: 5.56mm
    Weight: 5.65 lbs
    Range: 500 m
    Rate of fire: variable, depending on rate selected
    [/FONT]


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    [FONT=Verdana, Arial, Helvetica, sans-serif]M-24 Sniper Weapon [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]
    m24sniper.gif
    The M24 Sniper's Weapon System (SWS) represents a return to bolt action sniper rifles by the US Army. The rifle entered Army service in 1998. The M24 uses the Remington 700 action, although the receiver has been made for adaptation to take the .300 Winchester Magnum round. The stock (HS Precision) is made of a composite of Kevlar, graphite and fiberglass bound together with epoxy resins, and features aluminum bedding block and adjustable butt plate. A detachable bipod (Harris) can be attached to the stock's fore-end.
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The rifle is a bolt-action, six-shot repeating rifle (one round in the chamber and five rounds in the magazine). It is used with either the M3A telescope (day optic sight, usually called the M3A scope, a 10X fixed Leupold M3 Ultra telescope) or the metallic iron sight. [/FONT] [FONT=Verdana, Arial, Helvetica, sans-serif]This is the sniper weapon used by the Army[/FONT].
    [FONT=Verdana, Arial, Helvetica, sans-serif]Caliber: 7.62x51mm NATO (.308 win)
    Operation: Bolt Action
    Feed: 5-Round internal magazine
    Weight: 12.1 lb (5.49 kg) empty without telescope
    Length: 43in (1092mm)
    Sights: 10x42 Leupold Ultra M3A telescope sight (Mil-Dots), plus detachable emergency iron sights. (Redfield Palma International)
    Barrel: 24" length, 1 twist in 11.2", 5 lands & grooves.
    Stock: HS Precision - adjustable length.
    Max Effective Range: 800 meters (875 yards)
    Expected Accuracy: 1 MOA with M118 (Ammo is limiting factor)
    [/FONT]


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    [FONT=Verdana, Arial, Helvetica, sans-serif]M40A1 Sniper Rifle [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]
    m40.gif
    This is the preferred sniper rifle for the U.S. Marine Corps. The M40A1 sniper rifle is based on the Remington model 700. It is a heavy barrel, bolt action, magazine fed 7.62mm rifle that is optimized for accuracy with Match Grade ammunition. The rifle is equipped with a special 10 power Unertl sniper scope. With scope, the rifle weighs approximately 14.5 pounds. It is equipped with a built-in five round magazine.
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The unique characteristics of the M40A1 Sniper Rifle are: commercial competition-grade heavy barrel, McMillan fiberglass stock and butt pad, modified Winchester Model 70 floor plate and trigger guard, and modified and lightened trigger. In addition, each stock is epoxy bedded for accuracy and all weapons must shoot less than one minute of angle (MOA).[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The M40A1 was put into service in the 1970s to meet the need of a long range sniper rifle. Each rifle is hand built by specially trained and qualified personnel at the Marine Corps Marksmanship Training Unit (MTU) at Quantico, Virginia.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Length: 44 inches (111.76 centimeters)
    Barrel length: 24 inches (61 centimeters)
    Weight: 14.5 pounds (6.58 kilograms)
    Bore diameter: 7.62mm (.308 inches)
    Maximum effective range: 1000 yards (914 meters)
    Muzzle velocity: 2550 feet (777 meters) per second
    Chamber pressure: 50,000 psi
    Magazine capacity: 5 rounds
    Unit Replacement Cost: $2,105
    [/FONT]


    ////////////////////////////////////////////////////////////////////////////////////////////////////////////////////////////////////




    [FONT=Verdana, Arial, Helvetica, sans-serif]M-249 SAW [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]
    m249.jpg
    The M-249 is unofficially called the Minimi. The official name for the weapon is SAW which means Squad Automatic Weapon. Early test versions of the M-249 were plagued with problems, but the current model is considered reliable. The weapon entered Army service in 1987, replacing the M-60 Machine Gun.
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The M-249 is a .223 cal (5.56mm) gas operated light weight machine gun which feeds from a belt held in a 100 or 200 rounds box under the gun. This weapon has a plastic pistol grip and a folding stock so it can be kept compact and light. [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The M-249 machine gun is an ideal complementary weapon system for the infantry squad platoon. It is light enough to be carried and operated by one man, and can be fired from the hip in an assault, even when loaded with a 200-round ammunition box. The barrel change facility ensures that it can continue to fire for long periods. The US Army has conducted strenuous trials on the M249, showing that this weapon has a reliability factor that is well above that of most other small arms weapon systems. The weapon is used by the U.S. Army and the U.S. Marine Corps.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Type: Squad automatic weapon
    Entered service: 1987
    Specifications:
    Caliber: 5.56mm
    Length:100 cm
    Weight:16.3 lbs
    Range: 800 meters
    Rate of fire: 750 rounds per minute
    [/FONT]


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    [FONT=Verdana, Arial, Helvetica, sans-serif]M-240 Machine Gun[/FONT]


    [FONT=Verdana, Arial, Helvetica, sans-serif]
    m240.jpg
    The M-240 entered Army and Marine Corps service in 1997. The M-240 is a version of FN's MAG 58 general-purpose machine gun. The M-240 fires the 7.62mm NATO round and is very reliable, with an estimated 26,000 Mean Rounds Between Failure (MRBF).
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Advantages of this weapon include its popularity with other nation's forces and number of configurations. For example, in a helicopter crash, the M-240d helicopter-mount version could be quickly modified by installing the bipod and butt stock of the M-240b version, which would then allow the weapon to be used for self defense by the surviving helicopter crew members.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The M-240 is manufactured in the following configurations: M-240b is designed for infantry use. The "B" version weapon is equipped with a thermal shield over the rear of the barrel to protect the operator. The M-240c version is designed for use internally in M2/M3 Bradley Infantry Fighting Vehicle. The M-240d is designed for use on pintel mounts in helicopters and on the outside of tanks and armored vehicles. The M-240g version is used by special operations forces. The heat shield on this version is removed and there are special fittings for night sights.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Type: Medium machine gun
    Entered service: 1997
    Specifications:
    Caliber: 7.62mm
    Weight: 27.6 lbs
    Range: 1,100 m
    Rate of fire: 600-9 rounds per minute
    [/FONT]


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    [FONT=Verdana, Arial, Helvetica, sans-serif]M-9 Handgun[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Did you know that in combat, it's mostly officers who carry handguns? Most enlisted don't. Notable exceptions are military police, and special operations forces. The M-9 pistol is the primary sidearm for all of the military services. It entered the services in 1985 (1990 for the Army), pushing out the older M-1911A1 .45-caliber pistol, a weapon with an 80-year military history, and 4-inch-barrel, .38-caliber revolvers. The adoption of the M-9 pistol was the result of a congressional mandate to equip all U.S. services with a standard handgun. [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]
    m9-2.jpg
    The Colt-designed M-1911A1 served soldiers well in many wars; some older soldiers argued, why replace it? As with other Army weapons, competition proved the M-9 to be the best sidearm.
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]To get the nod, the M-9 had to meet strict requirements for functional reliability, speed of first shot, rapidity of fire, speed of reloading, range, penetration and accuracy to 50 yards. Also, the pistol's components had to be interchangeable, so a working weapon could be pieced together from the parts of others.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The M-9 went through a series of rugged tests to evaluate its functionality. An extreme climatic test checked its ability to withstand temperatures between minus 40 and 140 degrees. A 10-day salt water immersion and humidity trial tested its resistance to corrosion. It tackled mud, sand, dirt and water to test its operation under adverse field conditions. A fully loaded weapon was dropped four feet onto a hard surface to test for accidental discharge. [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]To test the ability to swap pistol components, testers fired and then disassembled 10 weapons. The parts were randomly put back together, then the weapons were fired again with no problems. If needed, the parts of weapons can be cannibalized to create a working pistol from broken ones.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Type: Semiautomatic pistol
    Entered Army service: 1990
    Specifications:
    Caliber: 9mm
    Length: 217mm
    Barrel length: 125mm
    Weight: 850 g
    Magazine capacity: 15 rounds
    Range: 50 m
    [/FONT]


    [FONT=Verdana, Arial, Helvetica, sans-serif]
    [/FONT]



    [FONT=Verdana, Arial, Helvetica, sans-serif]
    [/FONT]
     
    Last edited:

    chami t

    Junior member
  • Nov 22, 2008
    654
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    kandy
    [FONT=Verdana, Arial, Helvetica, sans-serif]M-2 Machine Gun[/FONT]
    zSB(3,3)


    [FONT=Verdana, Arial, Helvetica, sans-serif]
    m2.gif
    The Browning M2 .50 Caliber Machine Gun, Heavy barrel is an automatic, recoil operated, air-cooled machine gun with adjustable headspace and is crew transportable with limited amounts of ammunition over short distances. By repositioning some of the component parts, ammunition may be fed from either the left or right side. A disintegrating metallic link-belt is used to feed the ammunition into the weapon.
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]This gun is has a back plate with spade grips, trigger, and bolt latch release. This gun may be mounted on ground mounts and most vehicles as an anti-personnel and anti-aircraft weapon. The gun is equipped with leaf-type rear sight, flash suppressor and a spare barrel assembly. Associated components are the M63 antiaircraft mount and the M3 tripod mount.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The M-2 is used by all of the United States Military Services.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Builder: Saco Defense
    Length: 61.42 inches (156 centimeters)
    Weight:
    Gun: 84 pounds (38 kilograms)
    M3 Tripod (Complete): 44 pounds (19.98 kilograms)
    Total: 128 pounds (58 kilograms)
    Bore diameter: .50 inches (12.7mm)
    Maximum effective range: 2000 meters with tripod mount
    Maximum range: 4.22 miles (6.8 kilometers)
    Cyclic rate of fire: 550 rounds per minute
    Unit Replacement Cost: $14,002
    [/FONT]



    [FONT=Verdana, Arial, Helvetica, sans-serif]M-1014 Joint Service Combat Shotgun[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]
    jointserviceshotgun.jpg
    The Joint Service Combat Shotgun is a a compact, lightweight, semi-automatic, 12 gauge weapon configured with a standard magazine with a minimum capacity of six 2 3/4 inch cartridges. The Combat Shotgun is capable of firing 12 gauge 3.0 inch magnum ammunition and is interoperable with standard 2 3/4 inch ammunition without adjustment to the operating system.
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The M-1014 is constructed of lightweight polymer materials and corrosion resistant metal components. To enhance mission performance and provide increased operator flexibility, the M-1014 is equipped with modular components such as modular stocks in various configurations and modular barrels of various lengths.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The Marine Corps was the lead agency in the test and evaluation of this shotgun. It is designed to replace the many different shotguns used in all of the military service. The shotgun was officially accepted for production in 2001. The weapon is primarily used by security forces and by special operations forces. [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Caliber: 12 gauge, accepts 23/4" and 3" standard and magnum loads.
    Length: 39.8" w/stock extended, 34.9" collapsed.
    Weight: 8.44 lbs. empty.
    Safety: Ambidextrous manual cross bolt.
    Magazine Capacity: Six 3" shells seven 23/4", plus one chambered round can be unloaded without cycling through the action.
    Trigger Pull: 5.5 to 7.28 lbs.
    Buttstock: Modular telescopic with removable pistol grip.
    Sights: Adjustable aperture rear and fixed post front, radius 23.7"
    Maximum Effective Range: 40 yards with 00 buckshot and in excess of 100 yards with the rifled slug.
    [/FONT]


    [FONT=Verdana, Arial, Helvetica, sans-serif]
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]MP-5 Sub-Machine Gun[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]
    mp5.gif
    The MP5-N fires from a closed and locked bolt in either the automatic or semiautomatic modes. This gun is recoil operated and has a unique delayed roller locked bolt system, a retractable butt stock, a removable suppressor, and illuminating flashlight integral to the forward hand guard. The flashlight is operated by a pressure switch custom fitted to the pistol grip. This is the same basic weapon used by the FBI's Hostage Rescue Team and other world-class counter-terrorist organizations.
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The present inventory includes both suppressed and non-suppressed versions of the MP5. The basic configuration of this weapon makes for an ideal size, weight,and capable (accuracy, lethality, reliability, etc.) close quarters battle weapon system.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]This weapon is manufactured by Heckler and Koch and is presently fielded to Marine Corps Force Reconnaissance Companies and Marine Security Force Battalions, and Special Operations Units, such as Army Rangers, Delta Force, and Navy SEALS.. It is currently considered the main weapon in the close quarters battle (CQB) environment.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Length:
    Collapsed stock: 19.29 inches (49 centimeters)
    Extended stock: 25.98 inches (66 centimeters)
    Weight: 7.44 pounds (3.38 kilograms) (w/30 round magazine)
    Bore diameter: 9mm (.355 inches)
    Maximum effective range: 328.1 feet (100 meters)
    Rate of fire: 800 rounds per minute
    Unit Replacement Cost: $894
    [/FONT]


    [FONT=Verdana, Arial, Helvetica, sans-serif]
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Hand Grenades[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]
    m67grenade.gif
    Hand grenades are nothing more than small bombs,containing explosives or chemicals, that can be thrown by hand or rigged as booby traps. Their origin has been traced back many centuries, and it is generally agreed that the Chinese, whom we credit with the invention of gunpowder, were first to use them. However, it was not until World War I that they were sufficiently developed to be effective and safe. By World War II, the grenade inventory expanded to include smoke grenades for signaling and screening, phosphorus and fragmentation grenades to produce casualties, and gas grenades for both casualty and riot control effects. The grenades being used today are in many respects representative of the entire history of the development of grenades.
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]There are several varieties of hand grenades designed for many purposes. All of these grenades can be broadly classified into six general types: fragmentation, illumination, chemical, incendiary, smoke, and practice and training grenades.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The M67 fragmentation grenade is the standard grenade used by the U.S. Military. It has a smooth, sheet-metal body and is shaped like a ball. Its outer case is lined on the inside with a serrated wire recoil. It is filled with 6.5 ounces of an explosive, known as Composition B, and uses a detonating type of fuze. When the detonator causes Composition B to explode,fragments of the body and fuze assembly are hurled in all directions. The M67 weighs 14 ounces and the average man can throw it 40 meters. The effective casualty-producing radius is 15 meters.[/FONT]


    [FONT=Verdana, Arial, Helvetica, sans-serif]:):):):):):)
    [/FONT]​
     

    chami t

    Junior member
  • Nov 22, 2008
    654
    10
    18
    kandy
    bigger gun

    [FONT=Verdana, Arial, Helvetica, sans-serif]FIM-9 Stinger Missile[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]
    stinger.gif
    The Stinger weapon system is a man portable (34.5 pounds), shoulder-fired, supersonic missile system designed to counter high speed, low-level, ground attack aircraft. The Stinger is effective against helicopters, unmanned aerial vehicles, and observation and transport aircraft. Once fired, the Stinger uses proportional navigation algorithms to guide the missile to a predicted intercept point. The Stinger missile can be used as a man portable air defense system (MANPAD) when the weapon is fired from the gunner’s shoulder, mounted aboard the Avenger weapons system, or mounted in the light armored vehicle-air defense variant (LAV-AD).
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The Stinger is a true “fire and forget” missile, requiring no inputs from the gunner once the weapon is fired. This allows the gunner to take cover, move to an alternate position, or engage additional targets. The Stinger also possesses an integral identification, friend or foe (IFF) subsystem to assist the gunner in identifying friendly aircraft.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The launch motor ejects the missile from the launch tube. The missile coasts a safe distance (about 9 meters) from the gunner before the dual thrust flight motor ignites and provides a sustained 22 gravity acceleration that arms the missile. After the gunner arms the missile, a sustained flight phase maintains missile velocity until the propellant is consumed. Then the missile enters a free flight period in which the motor has burned out, but the missile maintains a degree of maneuverability prior to interception or self destruction.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The warhead consists of a fuze assembly and the equivalent of one pound of high explosives encased in a pyrophoric titanium cylinder. The fuze is extremely safe and makes the missile exempt from any hazards of electromagnetic radiation to ordnance conditions. The warhead can be detonated by penetrating the target, impacting the target, or self-destruction. Self-destruction occurs 15 to 19 seconds after launch.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Type: Short range air-defense missile
    Entered Army service: 1981
    Propulsion: Dual thrust solid fuel rocket motor
    Length: 5 feet (1.5 meters)
    Width: 5.5 inches (13.96 centimeters)
    Weight: 12.5 pounds (5.68 kilograms)
    Weight fully armed: 34.5 pounds (15.66 kg)
    Range: 1 to 8 kilometers
    Ceiling 10,000 feet (3.046 kilometers)
    Speed: Supersonic in flight
    Crew: 2 enlisted
    Guidance system: Fire-and-forget passive infrared seeker
    Warheads: High explosive
    Rate of fire: 1 missile every 3 to 7 seconds
    Sensors: Passive infrared
    Unit Replacement Cost $38,000
    Inventory: About 13,400 missiles available in the Army and Marine Corps
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]M-252 Mortar[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]
    m25.jpg
    The M252 81mm Medium Extended Range Mortar is a crew-served, medium weight mortar which is highly accurate and provides for a greater range (4,500 meters to 5,650 meters) and lethality than the previous 81mm mortar. The cannon has a crew-removable breech plug and firing pin. The muzzle end has a short tapered lead-in which acts as a blast attenuator device. The breech end is finned for better cooling. This mortar also uses the standard M64 mortar sight of the M-224 60mm mortar.
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The M252 is an adaptation of the standard British 81mm mortar developed in the 1970s. It is mostly commonly found in the mortar platoon of an Army or Marine Corps infantry battalion.

    The M252 is ideally suited to support airborne, air assault, mountain and light infantry units. The M-252 Mortar is used by the U.S. Army and the U.S. Marine Corps.
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Type: 81mm mortar
    Entered service: 1987
    Caliber: 81mm
    Barrel length:4 ft 6 in
    Weight: 91 lbs
    Range: 5,600 meters
    Rate of fire: 15 rounds/min sustained
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]M-224 Lightweight Mortar[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]
    m224mortar.gif
    The M224 60mm Lightweight Mortar is a smooth bore, muzzle loading, high-angle-of-fire weapon. The cannon assembly is composed of the barrel, combination base cap, and firing mechanism. The mount consists of a bipod and a base plate which is provided with screw type elevating and traversing mechanisms to elevate/traverse the mortar. The M64 sight unit is attached to the bipod mount via a standard dovetail. An additional short range sight is attached to the base of the cannon tube for firing the mortar on the move and during assaults. It has a spring-type shock absorber to absorb the shock of recoil in firing.
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The M224 replaced the older (WWII era) M2 and M19, 60mm Mortars. These weapons only possessed 2,200 yards of effective range. The M224 was designed to fire all types of the older ammunition, but its primary rounds are of the newer, longer-range type. The weapon is used primary by the U.S. Marine Corps.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Length: 40 inches (101.6 centimeters)
    Weight: 46.5 pounds (21.11 kilograms)
    Bore diameter: 60mm
    Maximum effective range: 2.17 miles (3490 meters)
    Rates of fire:
    Maximum: 30 rounds/minute
    Sustained: 20 rounds/minute
    Unit Replacement Cost: $10,658
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]AT4 Anti-Armor Weapon[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]
    at4.gif
    The M136 AT4 is the Army and Marine Corps's primary light anti-tank weapon. The M136 AT4 is a recoilless rifle used primarily by Infantry Forces for engagement and defeat of light armor. The recoilless rifle design permits accurate delivery of an 84mm High Explosive Anti-Armor warhead, with negligible recoil.
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The M136 AT4 is a lightweight, self-contained, anti armor weapon consisting of a free-flight, fin-stabilized, rocket-type cartridge packed in an expendable, one-piece, fiberglass-wrapped tube. The M136 AT4 is man-portable and is fired from the right shoulder only. The launcher is watertight for ease of transportation and storage. [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Though the M136 AT4 can be employed in limited visibility, the firer must be able to see and identify the target and estimate the range to it. Subsequent to the initial fielding of the weapon, a reusable night sight bracket was developed and fielded. It permits utilization of standard night vision equipment. The system's tactical engagement range is 250 meters and has been used in multiple combat situations. The round of ammunition is self-contained in a disposable launch tube. The system weighs 15 pounds and can be utilized effectively with minimal training. [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Primary function: Light anti-armor weapon
    Manufacturer: FFV Ordnance, Sweden and Alliant Techsystems
    Length: 40 inches (101.6 centimeters)
    Weight: 14.75 pounds (6.7 kilograms)
    Bore diameter: 84mm
    Maximum effective range: 984.3 feet (300 meters)
    Penetration: 400 mm of rolled homogenous armor
    Time of Flight (to 250 meters): less than 1 second
    Muzzle velocity: 950 feet (285 meters) per second
    Operating temperature: -104 to +140° F (-40 to +60° C)
    Ammunition: Rocket with shaped charge warhead
    Unit Replacement Cost: $1,480.64
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Multi-Purpose Assault Weapon[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]
    smaw.gif
    The Shoulder-Launched Multi-Purpose Assault Weapon (SMAW) is designed to destroy bunkers and other fortifications during assault operations as well as other designated targets with the dual mode rocket and to destroy main battle tanks with the HEAA rocket.
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif] The SMAW is an 83mm man-portable weapon system consisting of the MK153 Mod 0 launcher, the MK 3 Mod 0 encased HEDP rocket, the MK 6 Mod 0 encased HEAA rocket, and the MK217 Mod 0 spotting rifle cartridge. The launcher consists of a fiberglass launch tube, a 9mm spotting rifle, an electro-mechanical firing mechanism, open battle sights, and a mount for the MK42 Mod 0 optical and AN/PVS-4 night sights. The High Explosive, Dual Purpose (HEDP) rocket is effective against bunkers, masonry and concrete walls, and light armor. The High Explosive Anti-Armor (HEAA) rocket is effective against current tanks without additional armor. The 9mm spotting rounds are ballistically matched to the rockets and increase the gunner's first round hit probability. Training is accomplished with the MK7 Mod 0 encased common practice rocket and the MK213 Mod 0 noise cartridge.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif] The SMAW MK153 Mod 0 launcher is based on the Israeli B-300 and consists of the launch tube, the spotting rifle, the firing mechanism, and mounting brackets. The launch tube is fiberglass/epoxy with a gel coat on the bore. The spotting rifle is a British design and is mounted on the right side of the launch tube. The firing mechanism mechanically fires the spotting rifle and uses a magneto to fire the rocket. The mounting brackets connect the components and provide the means for boresighting the weapon. The encased rockets are loaded at the rear of the launcher. The spotting cartridges are stored in a magazine in the cap of the encased rocket.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Originally developed as a unique weapon for the U.S. Marine Corps, during Desert Storm, 150 launchers and 5,000 rockets were provided to the U.S. Army. The Army subsequently added the weapon to its inventory.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Primary function: Portable anti-armor rocket launcher.
    Length:
    To Carry: 29.9 inches (75.95 centimeters)
    Ready-to-Fire: 54 inches (137.16 cm)
    Weight:
    To Carry: 16.6 pounds (7.54 kg)
    Ready-to-Fire (HEDP): 29.5 pounds (13.39 kg)
    Ready-to-Fire (HEAA): 30.5 pounds (13.85 kg)
    Bore diameter: 83mm
    Maximum effective range:
    1 x 2 Meter Target: 250 meters
    Tank-Sized Target: 500 meters
    Introduction date: 1984
    Unit Replacement Cost: $13,000
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Dragon Weapon System[/FONT]
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    dragon.gif
    The Dragon Weapon System is designed to engage and destroy armor and light armored vehicles. The weapon is also effective against hard targets such as bunkers and field fortifications.
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The warhead power of Dragon makes it possible for a single Marine or soldier to defeat armored vehicles, fortified bunkers, concrete gun emplacements, or other hard targets. The launcher consists of a smoothbore fiberglass tube, breech/gas generator, tracker and support, bipod, battery, sling, and forward and aft shock absorbers. Non-integral day and night sights are required to utilize the Dragon.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif] The complete system consists of the launcher, the tracker and the missile, which is installed in the launcher during final assembly and received by the military in a ready to fire condition. The launch tube serves as the storage and carrying case for the missile. The night tracker operates in the thermal energy range.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The first-generation Dragon, a 1000-meter system requiring 11.2 seconds flight-to-target time, was developed for the US Army and fielded in 1970. A product improvement program (PIP) was initiated by the Marine Corps in 1985 and managed by NSWC Dahlgren. The PIP, designated Dragon II, was designed to increase warhead penetration effectiveness by 85%. The Dragon II missile is actually a retrofit of warheads to the first generation missiles already in the Marine Corps and Army inventory.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]TOW Missile System[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]
    towmissile.jpg
    The tube-launched, optically-tracked, wire-guided (TOW) missile is a crew-portable, vehicle-mounted, heavy anti armor weapon system consisting of a launcher and one of five versions of the TOW missile. It is designed to defeat armored vehicles and other targets such as field fortifications from ranges up to 3,750 meters. After firing the missile, the gunner must keep the crosshairs of the sight centered on the target to ensure a hit. The system will operate in all weather conditions in which the gunner can see a target throughout the missile flight by using either a day or night sight.
    The TOW system is used on the high mobility multipurpose wheeled vehicle (HMMWV), the M151 jeep, the armored personnel carrier, the Bradley Fighting Vehicle (BFV), COBRA helicopters, the Improved Tow Vehicle (ITV), and the USMC light armored vehicle. Three of the five TOW missile versions—Basic TOW, Improved TOW, and TOW 2—are no longer being produced for U.S. forces. However, these versions are used by 43 allied countries, and Switzerland co-produces the missile system. In the late 1980s, Hughes Aircraft Company, prime contractor for the TOW weapon system, began producing the TOW 2A which gave the system the capability of defeating reactive armor. The TOW 2B provides additional capability against future armored threats.
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]In May 1972, U.S. soldiers used the TOW in combat during the Vietnam War. This was the very first time that American troops had ever fired an American-made missile under wartime conditions. The system has also seen action in various clashes between Israel and Syria as well as during the Iran/Iraq war. The TOW was one of the earliest missile systems to arrive in Southwest Asia and proved to be highly effective throughout Operation Desert Storm.[/FONT]


    [FONT=Verdana, Arial, Helvetica, sans-serif]:shocked::shocked::shocked::shocked::shocked::shocked::shocked::shocked:
    [/FONT]​
     

    chami t

    Junior member
  • Nov 22, 2008
    654
    10
    18
    kandy
    some nifty individual equipment items

    [FONT=Verdana, Arial, Helvetica, sans-serif]AN/PVS-14 Night Vision Device [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]
    nightvision.gif
    AN/PVS-14 Monocular Night Vision Device (MNVD) is a light-weight, third generation night vision device that gives the soldier the operational advantage to “see at night.” NVDs (known also as Night Vision Goggles) are electro-optical devices that intensify (or amplify) existing light instead of relying on a light source of their own.
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The devices are sensitive to a broad spectrum of light, from visible through infrared. An accessory illuminator can increase the light available at the infrared end of the spectrum by casting a beam of light that is not visible to the human eye. When a soldier looks "through" a NVD, an amplified electronic image is seen on a phosphor screen, giving the soldier the ability to operate with little or no illumination from the moon, stars, or other ambient light sources. [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The PVS-14 system can be used with the head mount, as shown, or with a Kevlar helmet mount.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Field of View (degrees): 40 degrees
    Min Focus Range: 40 cm
    Weight (unit): 420 grams
    Infrared light emitting diode
    Automatic brightness protection
    Variable gain control knob
    Low battery indicator
    Power Source: 2) AA batteries (Alkaline)
    Operating temperature: -51 C to + 49 C
    Storage temperature: -51 C to + 85 C
    Immersion: 1 meter for 30 minutes
    [/FONT]


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    [FONT=Verdana, Arial, Helvetica, sans-serif]SINCGARS RT-1523E Radio[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]
    radio.gif
    The SINCGARS RT-1523E Advanced System Improvement Program (ASIP) Radio is the primary Combat Net Radio for the US Army, designated primarily for voice command and control for infantry, armor, and artillery units.
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The radio is a Single Channel Ground and Airborne Radio System which incorporates all the features of previous radio systems used with further enhancements to reduce it’s weight and size for the dismounted soldier and optimize its performance in the tactical internet. This is mainly due to the internal redesign of the radio and taking advantage of software based Digital Signal Processing (DSP) architecture. [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The ASIP radio is one-half the size and one-third the weight of the full size radio. With battery, handset and antenna, the total man pack weight is less than 9 lbs. The system is used for all inter-platoon communications. SINCGARS is capable of short-range or long-range operation for voice or digital communications. It can be used for single channel operation or in a jam-resistant, frequency-hopping mode that can be changed as needed. [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]30-88 MHz VHF-FM
    2320 Channels
    Single Channel and Frequency Hopping
    6 FH Presets (including TRANSEC keys)
    6 Single-channel Presets Plus Manual and Cue Channels
    Enhanced Data Mode (BPS) 1200, 2400, 4800, 9600
    Standard Data Mode (BPS) 600, 1200, 2400, 4800, 16,000
    Size: 3.4" high, 5.3" wide, and 10.15" deep
    33 Hr. Battery Life
    Embedded GPS Option
    Comprehensive Built-in Test Isolates Fault to Individual Module
    [/FONT]




    [FONT=Verdana, Arial, Helvetica, sans-serif]Mollie Vest[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]
    mollievest.gif
    MOLLE is an Army and Marine Corps item that replaces the aging ALICE (All-purpose, Lightweight, Individual Carrying Equipment) pack and Integrated Individual Fighting System introduced in 1988. One of the main components of the MOLLE system is the nylon mesh vest that has removable pockets to accommodate different carrying needs.
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif] Some of the new technology centers on the MOLLE's frame. Instead of the tubular aluminum used with the ALICE, a new anatomically-contoured frame made with plastic originally used in automobile bumpers has dramatically increased durability, functioning in temperatures ranging from -40 to 120 degrees F. MOLLE also advances load-carrying ability with its new suspension system. Heavily-padded shoulder straps and waist belt are adjustable for varying torso lengths, eliminating the two sizes of ALICE. More weight is distributed at the shoulders and hips, and during a prolonged road march, soldiers can shift the weight to where it feels more comfortable. Additionally, the Fighting Load Carrier (FLC) replaces the Load Bearing Equipment (LBE) web belt and suspenders of the ALICE. [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Soldiers and Marines can significantly increase the amount of ammunition they carry, and weight is evenly distributed across the torso. The vest has no metal clips or hooks that can be awkward and dig into the skin, and it has an H-harness in back to minimize heat buildup. It's adjustable to all sizes, and because the vest sits high, soldiers can fasten the MOLLE frame waist belt underneath the FLC to distribute some of the load to the hips. Three flap pockets on the FLC each hold two 30-round magazines, two grenade pockets and two canteen pouches.
    [/FONT]


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    [FONT=Verdana, Arial, Helvetica, sans-serif]Flak Vest[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]
    flakvest.gif
    Getting shot or hit by shrapnel can ruin your entire day in combat. In October of 2002, the Army and Marine Corps began issuing a new kevlar flak vest that is 35 percent lighter than the previous version. The 16.4-pound Interceptor system consists of a tactical vest and a pair of small arms protective inserts. The Kevlar vest includes detachable neck and groin guards, while the ceramic plates slide into pockets on the front and rear.
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]By itself, the Interceptor vest insulates a soldier from shrapnel and 9-mm pistol rounds. When the protective inserts are added, the system acts as a ballistic barrier to 7.62-mm rifle ammunition. The previous flak vest only offered protection against fragmentation. [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The Interceptor's inter-changeable components give troops the ability to dress to the level of a particular threat. Applications include combat operations, peace-keeping missions and field-training exercises. Regardless of the situation, Interceptor Body Armor functions as an effective defense against mines, grenades, mortar shells, artillery fire and rifle projectiles.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The Interceptor system allows commanders increased capability in the area's of survivability and maneuverability. Survivability due to the ability to withstand up to 7.62 mm hits and maneuverability due to the 8.7-pound weight savings of the new system.[/FONT]
     

    chami t

    Junior member
  • Nov 22, 2008
    654
    10
    18
    kandy
    [FONT=Verdana, Arial, Helvetica, sans-serif]Missiles. [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Tomahawk® Cruise Missile[/FONT]

    [FONT=Verdana, Arial, Helvetica, sans-serif]. The Tomahawk® is a long range, subsonic cruise missile used for land attack warfare, launched from surface ships and submarines.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The Tomahawk® cruise missiles are designed to fly at extremely low altitudes at high subsonic speeds, and are piloted over an evasive route by several mission tailored guidance systems. The first operational use was in Operation Desert Storm, 1991, with immense success. The missile has since been successfully used in several other conflicts. In 1995 the governments of the United States and United Kingdom signed a Foreign Military Sales Agreement for the acquisition of 65 missiles, marking the first sale of Tomahawk® to a foreign country. After a November 1998 launch and live warhead test, the U.K. declared operational capability. [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]
    tlam.gif
    The first production version of the Tomahawk® (known as "Block II") used a Terrain Contour Matching (TERCOM) and Digital Scene Matching Area Correlation (DSMAC) missile guidance system. In other words, the missile used a camera to look at the terrain it was following, and compared it to the terrain map in its memory. The 2nd generation (Block III) added a Global Positioning Satellite guidance capability to TERCOM and DSMAC.
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Radar detection of the missile is extremely difficult because of the small radar cross-section and low altitude. Tomahawk® has two warhead configurations: a 1,000-lb. blast/fragmentary unitary warhead and a general-purpose submunition dispenser with combined effect bomblets (cluster bombs). Because of its long range, lethality, and extreme accuracy Tomahawk® has become the weapon of choice for the U.S. Department of Defense. [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Tactical Tomahawk®, the next generation Tomahawk® cruise missile adds the capability to reprogram the missile while in-flight to strike any of 15 pre-programmed alternate targets or redirect the missile to any Global Positioning System (GPS) target coordinates. It also will be able to loiter over a target area, and with its on-board camera, will allow the warfighting commanders to assess target battle damage. Launched from the Navy's forward-deployed ships and submarines, Tactical Tomahawk®, will provide a greater flexibility to the on-scene commander. Tactical Tomahawk is projected to enter service in 2004.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Primary Function: long-range subsonic cruise missile for striking high value or heavily defended land targets.
    Contractor: Raytheon Systems Company, Tucson, Ariz.
    Unit Cost: approximately $600,000 (from last production contract)
    Power Plant: Williams International F107-WR-402 cruise turbo-fan engine; CSD/ARC solid-fuel booster
    Length: 18 feet 3 inches (5.56 meters); with booster: 20 feet 6 inches (6.25 meters)
    Weight: 2,900 pounds (1,315.44 kg); 3,500 pounds (1,587.6 kg) with booster
    Diameter: 20.4 inches (51.81 cm)
    Wing Span: 8 feet 9 inches (2.67 meters)
    Range: 870 nautical miles (1000 statute miles, 1609 km)
    Speed: Subsonic - about 550 mph (880 km/h)
    Guidance System: TERCOM, DSMAC, and GPS (Block III only)
    Warheads: 1,000 pounds or conventional submunitions dispenser with combined effect bomblets.
    Date Deployed: 11986 - IOC; 1994 - Block III; 2004 - Tactical Tomahawk®
    [/FONT]


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    agm86.jpg
    AGM - 86 Cruise Missiles.
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The AGM-86 Cruise Missile as specifically designed to be air-launched from Air Force B-52H bomber aircraft. There are two versions of the AGM-86. The AGM-86B (the first model produced) is a nuclear weapon. The AGM-86C is non-nuclear high explosive. While this feature is primarily concerned with non-nuclear weapons, in this case, we must also discuss the nuclear version, because the non-nuclear version was developed from the nuclear weapon.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]B-52H bombers carry six AGM-86 (either nuclear or non-nuclear) missiles on each of two externally mounted pylons and eight internally on a rotary launcher, giving the B-52H a maximum capacity of 20 missiles per aircraft. The small, winged AGM-86B/C missile is powered by a turbofan jet engine that propels it at sustained subsonic speeds. After launch, the missile's folded wings, tail surfaces and engine inlet deploy. The AGM 86C uses an onboard Global Positioning System (GPS) coupled with its inertial navigation system (INS) to fly. This allows the missile to guide itself to the target with pinpoint accuracy.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]In February 1974, the Air Force entered into contract to develop and flight-test the prototype AGM-86A air-launched cruise missile, which was slightly smaller than the later B and C models. The 86A model did not go into production. Instead, in January 1977, the Air Force began full-scale development of the AGM-86B, which greatly enhanced the B-52's capabilities and helped America maintain a strategic deterrent.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Production of the initial 225 AGM-86B missiles began in fiscal year 1980 and production of a total 1,715 missiles was completed in October 1986. The air-launched cruise missile had become operational four years earlier, in December 1982, with the 416th Bombardment Wing, Griffiss Air Force Base, N.Y., which deactivated when the base closed in 1995.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]In June 1986 a limited number of AGM-86B missiles were converted to carry a high-explosive blast/fragmentation warhead and an internal GPS. They were redesignated as the AGM-86C CALCM. This modification also replaced the B model's terrain contour-matching guidance system and integrated a GPS capability with the existing inertial navigation computer system.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The CALCM became operational in January 1991 at the onset of Operation Desert Storm. Seven B-52s, from Barksdale AFB, La., launched 35 missiles at designated launch points in the U. S. Central Command's area of responsibility to attack high-priority targets in Iraq. These "round-robin" missions marked the beginning of the air campaign for Kuwait's liberation and are the longest known aircraft combat sorties in history (more than 14,000 miles and 35 hours of flight).[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Prior to the 2nd Gulf War, CALCM's most recent employment occurred in Sept. 1996 during Operation Desert Strike. In response to Iraq's continued hostilities against the Kurds in northern Iraq, the Air Force launched 13 CALCMs in a joint attack with the Navy. This mission has put the CALCM program in the spotlight for future modifications.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]In 1996 and 1997, 200 additional CALCMs were produced from excess ALCMs. These missiles, designated Block I, incorporate improvements such as a larger and improved conventional payload (3,000 pound blast class), a multi-channel GPS receiver and integration of the buffer box into the GPS receiver. The upgraded avionics package was retrofitted into all existing CALCM (Block 0) so all AGM-86C missiles are electronically identical.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The AGM-86D CALCM Block II is equipped with a new Lockheed Martin 540 kg (1200 lb) AUP (Advanced Unitary Penetrator) penetrating warhead for use against deeply buried and/or hardened targets. The first flight test of an AGM-86D occurred in November 2001, and it is currently planned to produce almost 200 CALCMs as AGM-86Ds. [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Primary Function: Air-to-ground strategic cruise missile
    Contractor: Boeing Defense and Space Group.
    Guidance Contractors: Litton Guidance and Control, and Interstate Electronics Corp. (AGM-86C model)
    Power Plant: Williams Research Corp. F-107-WR-10 turbofan engine
    Thrust: 600 pounds
    Length: 20 feet, 9 inches (6.3 meters)
    Weight: 3,150 pounds (1,429 kilograms)
    Diameter: 24.5 inches (62.23 centimeters)
    Wingspan: 12 feet (3.65 meters)
    Range: AGM-86C: 600 nautical miles (nominal); classified (specific)
    Speed: AGM 86C, high subsonic (nominal), classified (specific)
    Guidance System: AGM 86C, Litton INS element integrated with multi-channel onboard GPS
    Warheads: AGM-86C; Block 0, 2,000 pound class, and Block I , 3,000 pound class
    Unit Cost: AGM-86B, $1 million; AGM-86C, additional $160,000 conversion cost
    Date Deployed: AGM-86C, January 1991
    Inventory: AGM-86C, 239, Block 0, 41; Block I, 198
    [/FONT]

    [FONT=Verdana, Arial, Helvetica, sans-serif]:):):):):):):):)
    [/FONT]​
     

    chami t

    Junior member
  • Nov 22, 2008
    654
    10
    18
    kandy
    [FONT=Verdana, Arial, Helvetica, sans-serif]AGM - 84D Harpoon.

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    [FONT=Verdana, Arial, Helvetica, sans-serif]
    harpoon.gif
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif] The AGM-84D Harpoon is an all-weather, over-the-horizon, anti-ship missile system produced by McDonnell Douglas. Its low-level, sea-skimming cruise trajectory, active radar guidance and warhead design assure high survivability and effectiveness.[/FONT] [FONT=Verdana, Arial, Helvetica, sans-serif]Originally developed for the Navy to serve as its basic anti-ship missile for fleetwide use (launched from Navy ships and submarines), the AGM-84D also has been adapted for use on the Air Force's B-52H bombers. The AGM-84D was first introduced in 1977, and in 1979, an air-launched version was deployed on the Navy's P-3 Orion aircraft.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]At the direction of Headquarters Strategic Air Command, the Harpoon Air Command and Launch Control Set was fully integrated into a fully operational B-52G from Mather AFB, Calif., in March 1983. Three successful live launches at the Naval Air Warfare Center, Point Mugu, Calif., led to the modification of a total of 30 B-52Gs with Harpoon launch control equipment, enough to provide two squadrons of Harpoon-capable B-52Gs by June 30, 1985. The 42nd Bombardment Wing, Loring Air Force Base, Maine, and the 43rd Bombardment Wing, Andersen Air Force Base, Guam, were first tasked to perform the Harpoon mission. Both wings refined tactics and doctrine to merge the long-range, heavy-payload capability of the B-52 with the proven reliability of this superior stand-off attack weapon.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]After Loring AFB closed and the retirement of the last B-52G at Castle AFB, Calif., the Harpoon mission was moved to the 2nd Bomb Wing at Barksdale AFB, La. Four B-52H models were rapidly modified (as an interim measure) to accept Harpoon launch control equipment pending B-52H fleet modification. Today, all B-52H aircraft are capable of carrying the HARM.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Primary Function: Air, surface, or submarine launched anti-surface (anti-ship) cruise missile.
    Contractor: The Boeing Company
    Power Plant: Teledyne Turbojet and solid propellant booster for surface and submarine launch.
    Thrust: 660 pounds (approximately 299.38 kilograms)
    Length: 12 feet, 7 inches (3.8354 meters) – air launched; 15 feet (4.572 meters) – surface and submarine launched.
    Weight: 1,145 pounds (519.372 kilograms) – air launched; 1,385 pounds (628.236 kilograms) – submarine or ship launched from box or canister launcher.
    Diameter: 13.5 inches (34.29 centimeters)
    Wing Span: 3 feet (91.44 centimeters) with booster fins and wings.
    Range: Over-the-horizon, in excess of 60 nautical miles.
    Speed: High Subsonic
    Guidance: Sea-skimming cruise monitored by radar altimeter, active radar terminal homing.
    Warhead: Penetration high-explosive blast (488 pounds/224 kilograms)
    Unit Cost: $720,000
    Date Deployed: 1985
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]
    slamer03.gif
    SLAM-ER.
    The Standoff Land Attack Missile - Expanded Response (SLAM-ER), an evolutionary upgrade to the combat-proven SLAM, is a day/night, adverse weather over-the-horizon, precision strike missile, used by the Navy and Marine Corps.
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]SLAM-ER addresses the Navy's requirements of a precision-guided Standoff Outside of Area Defense weapons. SLAM-ER extends the weapon system's combat effectiveness into the next century, providing an effective, long range, precision strike option for both pre-planned and Target of Opportunity attack missions against land and ship targets. Most significant among these enhancements are: a highly accurate, GPS-aided guidance system; improved missile aerodynamic performance characteristics that allow both greater range and more effective terminal attack profiles; a redesigned ordnance section for increased penetrating power and lethality; and a more user-friendly interface for both Man-in-the-Loop control and mission planning. SLAM-ER will be the first weapon to feature Automatic Target Acquisition (ATA), a revolutionary technological breakthrough which will automate and improve target acquisition in cluttered scenes, and overcome most countermeasures and environmentally degraded conditions.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]SLAM-ER roots go back to the original Harpoon anti-ship missile placed in the fleet in the late 1970s. Because of emerging operational requirements, missile for land attack was developed as a derivative of the Harpoon. The SLAM was developed and fielded in less than 48 months and was successfully employed by F/A-18 and A-6 aircrews in Desert Storm even before operational testing had begun. The potential of SLAM spurred further development of its standoff capabilities, to provide even greater improvements in range, accuracy, warhead penetration, dive angle and mission planning. Because of the Navy's growing focus on littoral warfare, SLAM-ER program initiatives were formalized in December 1994 when the Assistant Secretary of the Navy for Research, Development and Acquisition gave the go ahead to proceed with engineering and manufacturing development and accelerate SLAM-ER production and deployment to the fleet.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Primary Function: long range, air-launched precision land attack cruise missile
    Contractor: The Boeing Company
    Power Plant: Teledyne Turbojet and solid propellant booster for surface and submarine launch.
    Thrust: greater than 600 pounds (greater than 272.16 kg)
    Length:14 feet 4 inches (4.36 meters)
    Weight:1,400 pounds (635.04 kg)
    Diameter: 13.5 inches (34.29 centimeters)
    Wing Span: 7.158 feet (2.1819 meters)
    Range: Over-the-horizon, in excess of 150 nautical miles (277.95 km)
    Speed: High Subsonic
    Guidance: ring laser gyro Inertial Navigation System (INS) with multi-channel GPS; infrared seeker for terminal guidance with Man-in-the-Loop control data link from the controlling aircraft. Upgraded missiles will incorporate Automatic Target Acquisition (ATA)
    Unit Cost: $500,000
    Date Deployed: mid 1999
    [/FONT]
     

    chami t

    Junior member
  • Nov 22, 2008
    654
    10
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    kandy
    [FONT=Verdana, Arial, Helvetica, sans-serif]
    agm-130.jpg
    AGM-130 Missile.
    The AGM-130, used by the Air Force, is a powered air-to-surface missile designed for high- and low-altitude strikes at standoff ranges against a variety of targets.
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Carrying forward the modular concept of the GBU-15 guided weapon system, the AGM-130 employs a rocket motor for extended range and an altimeter for altitude control. The AGM-130 provides a significantly increased standoff range beyond that of the GBU-15.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The AGM-130 is equipped with either a television or an imaging infrared seeker and data link. The seeker provides the launch aircraft a visual presentation of the target as seen from the weapon. During free flight this presentation is transmitted by the AXQ-14 data-link system to the aircraft cockpit monitor.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The seeker can be either locked onto the target before or after launch for automatic weapon guidance, or it can be manually steered by the weapon systems officer. Manual steering is performed through the two-way data link.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The AGM-130 is designed to be used with F-15E aircraft. Development of the AGM-130 began in 1984 as a product improvement of the GBU-15 guided glide bomb.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]For the primary mode of operation, the aircraft flies to a pre-briefed launch position. Survivability of aircraft and crew is enhanced by launching the weapon at low altitude and significant standoff range, thus avoiding detection by enemy air defenses. After launch, the weapon flies through glide-powered-glide phases toward the target area with midcourse guidance updates provided by global positioning system (GPS) navigational information or through the data link. [/FONT][FONT=Verdana, Arial, Helvetica, sans-serif] Upon termination of the powered flight phase the rocket motor is ejected. As the target comes into view, the weapon systems officer has dual flexibility in guiding the weapon via the data link. For automatic terminal homing, the guidance tracker is locked on target but can be manually updated for precision bombing. When total manual guidance is used, the operator manually guides the weapon to the target aimpoint. For those aircraft not equipped with a data-link pod, the weapon may be launched in the direct attack mode.
    [/FONT] [FONT=Verdana, Arial, Helvetica, sans-serif]Primary Function: Air-to-surface guided and powered bomb (missile)
    Contractor: Boeing Co.
    Thrust: Classified
    Length: 12 feet, 10.5 inches (3.90 meters)
    Launch Weight: 2,917 pounds (1,312.65 kilograms)
    Diameter: 18 inches (45.72 centimeters)
    Wingspan: 59 inches (149.86 centimeters)
    Range: Classified
    Ceiling: 30,000-plus feet (9,091 meters)
    Speed: Classified
    Guidance System: television or imaging infrared seeker
    Date Deployed: 1994
    Unit Cost: Approximately $450,000 per weapon
    Inventory: Classified.
    [/FONT]


    [FONT=Verdana, Arial, Helvetica, sans-serif]General Purpose Bombs.[/FONT][FONT=Verdana, Arial, Helvetica, sans-serif] [/FONT]

    [FONT=Verdana, Arial, Helvetica, sans-serif][/FONT]
    zSB(3,3)


    [FONT=Verdana, Arial, Helvetica, sans-serif]
    mk-82.gif
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]General Purpose (GP) bombs are free fall ordnance or sometimes referred to as dumb bombs. The bombs are dumb in the fact they are only as accurate as the pilot or platform delivering them. The primary weapons effects are due to blast and fragmentation. [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]They come in a variety of sizes and weights ranging from 250 pounds for the MK-81 (pronounced "Mark"), 500 pounds for the MK-82, 1000 pounds for the MK-83, 2,000 pounds for the MK-84, 750 pounds for the M-117, and 3000 pounds for the M-118. Obviously the bigger the bomb the bigger the bang. [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]An improved 2,000 pounder designated the BLU-109/B has twice the thickness of the MK-84 and is used as a hardened penetration bomb. The BLU-107/B DURANDAL is a French made runway penetration bomb used for cratering runways rendering useless for aircraft operations. The M-117 (750 lbs) and M-118 (3000 lbs) bombs are primarily carried by heavy bombers. [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]By adding special guidance kits to the MK-83 and MK-84 the bombs accuracy and performance are greatly enhanced. These bombs then become precision guided munitions (smart bombs) and are designated by the GBU (Guided Bomb Unit) series bombs.[/FONT]


    [FONT=Verdana, Arial, Helvetica, sans-serif]
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]
    jdam.jpg
    Joint Direct Attack Munitions (JDAM).

    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]JDAM isn't exactly a bomb. It's a kit which turns a dumb bomb into a smart bomb. The Joint Direct Attack Munition (JDAM) is a guidance tail kit that converts existing unguided free-fall bombs into accurate, adverse weather "smart" munitions. With the addition of a new tail section that contains an inertial navigational system and a global positioning system guidance control unit, JDAM improves the accuracy of unguided, general purpose bombs in any weather condition. JDAM is a joint U. S. Air Force and Department of Navy program. [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]JDAM is a guided air-to-surface weapon that uses either the 2,000-pound BLU-109/MK 84 or the 1,000-pound BLU-110/MK 83 warheads as the payload. JDAM enables employment of accurate air-to-surface weapons against high priority fixed and relocatable targets from fighter and bomber aircraft. Guidance is facilitated through a tail control system and a GPS-aided INS. The navigation system is initialized by transfer alignment from the aircraft that provides position and velocity vectors from the aircraft systems.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Once released from the aircraft, the JDAM autonomously navigates to the designated target coordinates. Target coordinates can be loaded into the aircraft before takeoff, manually altered by the aircrew before weapon release, and automatically entered through target designation with onboard aircraft sensors. In its most accurate mode, the JDAM system will provide a weapon circular error probable of 13 meters or less during free flight when GPS data is available. If GPS data is denied, the JDAM will achieve a 30-meter CEP or less for free flight times up to 100 seconds with a GPS quality handoff from the aircraft. [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]JDAM can be launched from very low to very high altitudes in a dive, toss and loft or in straight and level flight with an on-axis or off-axis delivery. JDAM enables multiple weapons to be directed against single or multiple targets on a single pass.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]JDAM is currently compatible with B-1B, B-2A, B-52H, F-16C/D and F/A-18C/D aircraft. Follow-on integration efforts are currently underway or planned to evaluate compatibility with the A-10 F-15E, F-22, F-117, AV-8B, F-14A/B/D, F/A-18E/F, S-3, and the Joint Strike Fighter.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Desert Storm highlighted a shortfall in air-to-surface weapon capability. Adverse weather conditions limited employment of precision guided munitions. Unguided weapon accuracy was also degraded when delivered from medium and high altitudes. Research and development of an"adverse weather precision guided munition" began in 1992. The first JDAMs were delivered in 1997 with operational testing conducted in 1998 and 1999. More than 450 JDAMs were dropped during testing, recording an unprecedented 95 percent system reliability while achieving a 9.6-meter accuracy rate. JDAM performance has been demonstrated in operationally representative tests including drops through clouds, rain and snow. These tests included a B-2 releasing 16 JDAMs on a single pass against multiple targets in two separate target areas. [/FONT][FONT=Verdana, Arial, Helvetica, sans-serif] JDAM and the B-2 made their combat debuts during Operation Allied Force. The B-2s, flying 30-hour, nonstop, roundtrip flights from Whiteman Air Force Base, Mo., delivered more than 600 JDAMs during Allied Force. This combination of stealth and accuracy has revolutionized air warfare. Growth of the JDAM family of weapons expanded to the MK-82 500-pound version, which began development in late 1999. Also, the Navy is currently studying the effects of adding enhancements such as improved GPS accuracy, a precision seeker for terminal guidance and additional warheads.
    [/FONT] [FONT=Verdana, Arial, Helvetica, sans-serif]Primary Function: Guided air-to-surface weapon
    Contractor: Boeing Corp.
    Length: (JDAM and warhead) GBU-31 (v) 1/B: 152.7 inches (387.9 centimeters); GBU-31 (v) 3/B: 148.6 inches (377.4 centimeters); GBU-32 (v) 1/B: 119.5 inches (303.5 centimeters)
    Launch Weight: (JDAM and warhead) GBU-31 (v) 1/B: 2,036 pounds (925.4 kilograms); GBU-31 (v) 3/B: 2,115 pounds (961.4 kilograms); GBU-32 (v) 1/B: 1,013 pounds (460.5 kilograms)
    Wingspan: GBU-31: 25 inches (63.5 centimeters); GBU-32: 19.6 ins. (49.8 centimeters)
    Range: Up to 15 miles
    Ceiling: 45,000-plus feet (13,677 meters)
    Guidance System: GPS/INS
    Unit cost: Approximately $21,000 per tailkit (FY 01 dollars)
    Date Deployed: 1999
    Inventory: The tailkit is in full-rate production. Projected inventory is 87,496 total, 62,000 for the Air Force and 25,496 for the Navy
    [/FONT]
     

    chami t

    Junior member
  • Nov 22, 2008
    654
    10
    18
    kandy
    [FONT=Verdana, Arial, Helvetica, sans-serif]GBU-10/12 Paveway II.

    [/FONT][FONT=Verdana, Arial, Helvetica, sans-serif][/FONT] [FONT=Verdana, Arial, Helvetica, sans-serif]
    gbu-12.jpg
    Based on the MK-82 & MK-84 GP bombs, the Paveway II series of Laser Guided Bombs (LGBs) contains a semi-active laser homing seeker, canards on the nose & tail section, and control surfaces on the aft end. The weapon is capable of operating in cloud ceilings down to 2,500 feet. The GBU-10/12 weigh 2,081 lbs & 610 lbs, respectively.
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]GBU-10[/FONT][FONT=Verdana, Arial, Helvetica, sans-serif]
    Class 2000 lb. Paveway I & II Laser Guided Weapons
    Mission Air interdiction
    Targets Mobile hard, fixed soft, fixed hard
    Service Air Force, Navy
    First capability 1976
    Guidance method Laser
    Weight (lbs.) 2562
    Length: (in.) 172
    Diameter (in.): 15/18 (Warhead)
    28 (Airfoil Group)
    Warhead: BLU-109 penetrator
    MK 84: Blast/Fragmentation
    Explosive: 535 lbs. Tritonal [BLU-109]
    945 lbs. Tritonal [MK 84]
    Range: 8 nautical miles
    Circular error probable: 9 meters
    Quantity: Air Force: 10,145
    Navy: 1,184
    Production unit cost: Air Force: $23,700
    Navy: $26,100
    Platforms: A-7, A-10, B-52, F-111, F-117, F-15E, F- 16 , F/A-18 C/D, A-6, F-14
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]GBU-12
    Class: 500 lb. Paveway I & II Guided Weapon
    Mission: Air interdiction
    Targets: Mobile hard, fixed soft, fixed hard
    Service: Air Force, Navy
    Contractor: Texas Instruments
    First capability: 1976
    Guidance: Semi-Active Laser
    Weight: (lbs.) 800
    Length (in.): 129
    Diameter (in.): 11 (Warhead); 18 (Airfoil Group)
    Warhead: MK-82 Blast/Fragmentation
    Explosive: Tritonal, PBXN-109 (192 lbs.)
    Range: 8 nautical miles
    Circular error probable: 9 meters
    Quantity: Air Force: 29,654
    Navy: 2,982
    Production unit cost: Air Force: $19,000;
    Navy: $19,050
    Platforms: A-7, A-10, B-52, F-111, F-117, F-15, F- 16, F/A-18 C/D, F-14, A-6
    [/FONT]


    [FONT=verdana, geneva, helvetica]Bombs [/FONT] zSB(3,3)


    [FONT=Verdana, Arial, Helvetica, sans-serif]
    gbu15.gif
    GBU-15.
    The GBU-15 bomb is an unpowered, glide weapon used to destroy high value enemy targets. It is designed to be used with F-15E and F-111F aircraft. The weapon consists of modular components that are attached to either an MK-84 or BLU-109 penetrating warhead. Each weapon has five components -- a forward guidance section, warhead adapter section, control module, airfoil components and a weapon data link.
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The guidance section is attached to the nose of the weapon and contains either a television guidance system for daytime or an imaging infrared system for night or limited, adverse weather operations. A data link in the tail section sends guidance updates to the control aircraft that enables the weapon systems operator to guide the bomb by remote control to its target. The umbilical receptacle passes guidance and control data between cockpit control systems of the launching aircraft and the weapon prior to launch. The rear control section consists of four wings are in an X-like arrangement with trailing edge flap control surfaces for flight maneuvering. [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The control module contains the autopilot, which collects steering data from the guidance section and converts the information into signals that move the wing control surfaces to change the weapons flight path. The GBU-15 may be used in direct or indirect attack. In a direct attack, the pilot selects a target before launch, locks the weapon guidance system onto it and launches the weapon. The weapon automatically guides itself to the target, enabling the pilot to leave the area. In an indirect attack, the weapon is guided by remote control after launch. The pilot releases the weapon and, via remote control, searches for the target. [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Once the target is acquired, the weapon can be locked to the target or manually guided via the data-link system. This highly maneuverable weapon has an optimal, low-to-medium altitude delivery capability with pinpoint accuracy. It also has a standoff capability. Desert Storm F-111F pilots used GBU-15 glide bombs to seal flaming oil pipeline manifolds sabotaged by Saddam Hussein's troops.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Primary Function: Air-to-surface guided glide bomb.
    Mission: Offensive counter air, close air support, interdiction, naval anti- surface warfare
    Targets: Mobile soft, fixed hard, fixed soft
    Service: Air Force
    Contractor: Rockwell International Corp.
    First capability: 1983
    Guidance System: Television Electro Optical TV via Mid-course guidance Beacon Data Link
    Launch Weight: 3640 lbs
    Length: 12 feet, 10.5 inches (3.91 meters)
    Diameter: 18 inches (0.45 meters)
    Wingspan: 4 feet, 11 inches (1.49 meters)
    Range: Greater than 5 nautical miles
    Ceiling: 30,000-plus feet (9,091 meters)
    Speed: Classified
    Warheads: Mk-84 general purpose or
    BLU-109 penetrating bombs
    Explosive: 945 Lbs. Tritonal[Mk-84]
    535 Lbs. Tritonal [BLU-109]
    Production unit cost: $195,000
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]
    gbu-24.gif
    GBU-24 Paveway III.
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif] The GBU-24 is a third generation laser guided bomb, called the Paveway III, and contains a penetrating warhead. The bomb is a precision guided munition effective against a broad range of high-value targets. It can be employed from various altitudes to include low, medium, and high altitude operations. The Paveway III was developed by Texas Instruments and is employed by the F-111, F-15E, and F-16. The GBU-24s performance was proved successfully during the Gulf War, and it remains in production. [/FONT][FONT=Verdana, Arial, Helvetica, sans-serif] The Paveway III uses semiactive laser homing to guide to its target, and has an advanced guidance section with an adapted high lift airframe to improve stability and performance. The system provides operational flexibility with the use of an adaptive auto pilot feature, along with a very sensitive scanning seeker. The entire bomb weighs 2,350 pounds and is approximately 14 feet long.
    [/FONT] [FONT=Verdana, Arial, Helvetica, sans-serif]Mission: Close air support, interdiction, offensive counter air, naval anti- surface warfare
    Targets: Mobile hard, fixed soft, fixed hard
    Service: Air Force, Navy
    First capability: 1983
    Guidance method: Laser
    Range: Greater than 10 nautical miles
    Production unit cost: $55,600
    Quantity: 13,114
    Platforms: A-6, A-10, F-14, F-15, F-16, F/A-18, F-111
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]
    gbu27.gif
    GBU-27.
    The GBU-27 is a 2,200 pound laser-guided bomb designed specifically for use by the F-117 Stealth Fighter. It is a highly accurate, hard-structure munition compatible with the F-117's advanced target acquisition/designator system. The GBU-27 uses a BLU-109 improved performance 2,000 pound bomb developed in 1985 under the project name HAVE VOID. The BLU-109 was designed for use against hardened structures and features a high-strength forged steel case and a new delayed-action tail fuze. It carries 550 pounds of high explosives and can penetrate more than six feet of reinforced concrete before exploding.
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The GRU-27 uses a modified Paveway II guidance control unit which provides "terminal trajectory shaping" for optimum impact angle against various target structures. For example, it will hit an aircraft shelter with a vertical impact, but make a horizontal approach to a bridge support. A Paveway II tail assembly with folding wings completes the bomb. [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The F-117 can carry two GBU-27s in two weapons bays and is reportedly capable of hitting a one square meter target from an altitude of 25,000 feet. The GBU-27 was used extensively during Desert Storm, with a claimed hit probability of over 95 percent. [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Mission: Close air support, interdiction, offensive counter air, naval anti- surface warfare
    Targets: Mobile hard, fixed hard, fixed soft
    Service: Air Force
    First capability: 1987
    Guidance method: Laser
    Range: Greater than 10 nautical miles
    Production unit cost: $55,000
    Quantity: 3,213
    Platform: F-117
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]
    gbu-28.jpg
    GBU-28.
    The GBU-28 is the famed bunker buster used in Desert Storm. It was developed in minimal time under USAF's rapid response program. It is primarily used as a deep penetration weapon against buried and hardened command and control facilities. The bomb is essentially an Army 8 inch howitzer modified with a GBU-27 guidance kit to produce a 4,700 pound laser guided bunker busting bomb. Lockheed Missile and Space System was the contractor on the project. Two GBU-28s were dropped in Desert Storm by F-111s but has been flight tested for use on the F-15E too. Advanced versions to improve operational capability and flexibility are being studied.
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Mission: Offensive counter air, close air support, interdiction
    Targets: Fixed hard
    Class: 4,000 lb. Penetrator, Blast/Fragmentation
    Service: Air Force
    Contracto:r Lockheed (BLU-113/B), National Forge (BLU-113A/B),
    First capability: 1991
    Weight (lbs.): 4,414
    Length (in.): 153
    Diameter (in.): 14.5
    Explosive: 6471bs. Tritonal
    Guidance: method Laser
    Range: Greater than 5 nautical miles
    Production unit cost: $145,600
    Quantity: 125 plus additional production
    Platforms: F-15E, F-111F
    [/FONT]

    [FONT=Verdana, Arial, Helvetica, sans-serif]
    [/FONT]
     

    chami t

    Junior member
  • Nov 22, 2008
    654
    10
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    kandy
    [FONT=Verdana, Arial, Helvetica, sans-serif]
    daisycutter.jpg
    BLU-82B Daisy Cutter.
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]
    [/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The Daisy Cutter was first used by the Air Force in the final year of U.S. involvement in the Vietnam War for clearing thick jungle areas to create instant landing zones for Army helicopters. Air Force documents call the BLU-82B weapon system “Commando Vault.”[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]It is a general-purpose “dumb bomb” loaded aboard newer versions of the C-130 Hercules, a four-engine workhorse used by the Air Force for more than 30 years.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]Because the bomb lacks a tail fin assembly, the same parachute that pulls the weapon from the back of the C-130 keeps its nose down as it falls.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]The warhead contains 12,600 pounds of explosives and is detonated just above the ground by a 38-inch fuse probe extending from the bomb’s nose.[/FONT]
    [FONT=Verdana, Arial, Helvetica, sans-serif]It produces enough power to level trees and buildings. [/FONT][FONT=Verdana, Arial, Helvetica, sans-serif] Eleven BLU-82s were dropped during Operation Desert Storm, all from special operations C-130s known as Combat Talons.
    The initial drops were intended to test the bomb’s ability to clear mines; however, no reliable assessment was completed because the war didn’t last long enough.
    The crew of a MC-130E Combat Talon special operations airplane dropped a BLU-82 bomb near an Iraqi position.
    The bomb detonated in an explosion that momentarily lit up the entire front.
    A leaflet drop warned Iraqi soldiers more such bombs would be dropped on their positions; the threat was believed to be responsible for mass defections, including almost all of one Iraqi battalion’s staff.
    Class: 15,000 lb. Blast
    Guidance: Ballistic
    Autopilot: None
    Propulsion: None
    Weight (lb.): 15,000
    Length (in): 141.6
    Diameter (in): 54
    Warhead (lbs.): 15,000
    Explosive:Aluminum Powder (12,600 lbs.)
    Fuze: M904 (Nose); M905 (Tail)
    Unit Cost: $27,318
    Aircraft: MC-130
    [/FONT]
     

    chami t

    Junior member
  • Nov 22, 2008
    654
    10
    18
    kandy
    AIRCRAFT :shocked:
    laser gunship



    laser_gunship.jpg




    polecat_lockeed_martin.jpg

    Lockeed Martin's


    offwhite_line350.jpg

    fa22raptor.jpg


    The $155 Million F/A-22 Raptor the Ultimate Stealth Fighter

    mq-9_predator.jpg

    MQ-9 Predator UAV
    predator_loaded.jpg

    MQ-9 Predator fully loaded with weapons

    shadow200_drone.jpg


    :oo: :oo: :oo:

     
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