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AGM-114 Hellfire - Wikipedia, the free encyclopedia

AGM-114 Hellfire

From Wikipedia, the free encyclopedia

AGM-114 Hellfire

A model of a Hellfire's components
Type Air-to-surface and surface-to-surface missile
Production history
Manufacturer Lockheed Martin
Specifications
Length 64 in (163 cm)
Diameter 7 in (17.8 cm)

Warhead High Explosive Anti-Tank (HEAT); 20 lb (9 kg) tandem anti-armor
Metal Augmented Charge (MAC); 18 lb (8 kg) shaped-charge
Blast Fragmentation

Engine Solid-fuel rocket
Wingspan 13 in (33 cm)
Operational
range
546 yd – 5 mi (500 m – 8 km)
Speed Mach 1.3 (950 mph; 425 m/s)
Guidance
system
Semi-active laser homing
millimeter wave radar seeker
Launch
platform
Rotary- and fixed-wing platforms, Unmanned aerial vehicle, tri-pods, ships, and ground vehicles

The AGM-114 Hellfire is a multi-platform, multi-target U.S. modular missile system.

Contents

[edit] Description

The development of the Hellfire Missile System began in 1974 with the US Army requirement for a "tank-buster", launched from helicopters to defeat armored vehicles.[1] Production of the AGM-114A started in 1982. The Development Test and Evaluation (DT&E) launch phase of the AGM-114B took place in 1984. The DT&E on the AGM-114K was completed in Fiscal Year (FY)93 and FY94. AGM-114M did not require a DT&E because it is the same as the AGM-114K except for the warhead. The early variants were laser guided with recent variants being radar guided. The Hellfire has matured into a comprehensive weapon system capable of being deployed from rotary- and fixed-wing aircraft, naval assets and land-based systems against a variety of targets.

Hellfire II, developed in the early 1990s is a modular missile system with several variants for maximum battlefield flexibility. Hellfire II's semi-active laser variants (AGM-114K high-explosive anti-tank (HEAT), AGM-114KII with external blast frag sleeve, AGM-114M [blast fragmentation], and AGM-114N metal augmented charge [MAC]) achieve pinpoint accuracy by homing in on a reflected laser energy beam aimed at the target from the launching platform. Predator and Reaper UAVs carry the Hellfire II, but the most common platform is the AH-64 helicopter gunship, which can carry up to sixteen of the missiles at once. The AGM-114L, or Longbow Hellfire, is a fire-and-forget weapon: equipped with a millimeter wave (MMW) radar seeker, it requires no further guidance after launch and can hit its target without the launcher being in line of sight of the target. It also provides capability in adverse weather and battlefield obscurants. Each Hellfire weighs 47 kg / 106 pounds, including the 9 kg / 20 pound warhead, and has a range of 8,000 meters. As of late 2007, some 21,000 Hellfire IIs have been built since 1990, at a cost of about $68,000 each.

The Joint Common Missile (JCM) was to replace Hellfire II (along with the AGM-65 Maverick) by around 2011. The JCM was developed with a tri-mode seeker and a multi-purpose warhead that would combine the capabilities of the several Hellfire variants. In the budget for FY2006, the US Department of Defense canceled a number of projects that they felt no longer warranted continuation based on their cost effectiveness, including the JCM, although some military and industry sources have produced data showing JCM is the most cost-effective way of adding performance on a timely basis across multiple platforms to meet projected threat growth. A possible new procurement for a JCM successor called the Joint Air to Ground Missile (JAGM) is under consideration. Due to the U.S. military's continuing need for a proven precision-strike aviation weapon in the interim until a successor to the JCM is fielded, as well as extensive foreign sales, it is likely the Hellfire will continue to remain in service for many years to come.

[edit] Combat history

Since being fielded, Hellfire missiles have proven their effectiveness in combat in Operation Just Cause in Panama, Operation Desert Storm, Operation Allied Force in Kosovo, Operation Enduring Freedom in Afghanistan, and most recently, Operation Iraqi Freedom—where they have been fired successfully from Apache and Cobra attack helicopters, Kiowa scout helicopters, and Predator unmanned aerial vehicles (UAVs). The Israeli Defence Forces have used them extensively against Palestinian targets.

Between 2001 and 2007, the U.S. has fired over 6,000 Hellfires in combat. The US military has found the missile effective in urban areas as the relatively small warhead reduces the risk of civilian casualties. The laser guidance means that, together with some luck, a skilled operator can put a missile through the window of a building.

[edit] Launch vehicles and systems

Hellfire loaded onto the rails of a United States Marine Corps AH-1W Super Cobra at Balad Air Base in Iraq in 2005.
Hellfire loaded onto the rails of a United States Marine Corps AH-1W Super Cobra at Balad Air Base in Iraq in 2005.

The system has been tested for use on the High Mobility Multipurpose Wheeled Vehicle (HMMWV) and the Improved TOW Vehicle (ITV). Test shots have also been fired from a C-130 Hercules (see photos below). Sweden and Norway use the Hellfire for coastal defense, and Norway has conducted tests with Hellfire launchers and aiming stations mounted on the Stridsbåt 90 coastal assault boat[2].

[edit] Operators

[edit] Variants

[edit] AGM-114A Basic Hellfire

[edit] AGM-114B/C Basic Hellfire

  • M120E1 low smoke motor.
  • AGM-114B has electronic SAD (Safe/Arming Device) for safe shipboard use.
  • Unit cost: $25,000

[edit] AGM-114D/E Basic Hellfire

  • Proposed upgrade of AGM-114B/C with digital autopilot—not built.

[edit] AGM-114F Interim Hellfire

  • Target: Tanks, armored vehicles.
  • Range: 7,000 m (7,650 yd)
  • Guidance: Semi-active laser homing.
  • Warhead: 9 kg (20 lb) tandem shaped charge HEAT.
  • Length: 180 cm (71 in)
  • Weight: 48.5 kg (107 lb)

[edit] AGM-114G Interim Hellfire

  • Proposed version of AGM-114F with SAD—not built.

[edit] AGM-114H Interim Hellfire

  • Proposed upgrade of AGM-114F with digital autopilot—not built.

[edit] AGM-114J Hellfire II

  • Proposed version of AGM-114F with lighter components, shorter airframe, and increased range—not built.

[edit] AGM-114K Hellfire II

A Hellfire II cross-sectioned.
A Hellfire II cross-sectioned.
  • Target: All armored threats
  • Range: 8.000 m (8,749 yd)
  • Guidance:
    • Semi-active laser homing
    • Digital autopilot
    • Electro-optical countermeasures hardening
    • Target reacquisition after lost laser lock
  • New electronic SAD
  • Warhead: 9 kg (20 lb) tandem shaped charge HEAT
  • Length: 163 cm (64 in)
  • Weight: 45 kg (99 lb)
  • Unit cost: $65,000
  • Essentially the proposed AGM-114J w/ SAD

[edit] AGM-114L Longbow Hellfire

  • Target: All armored threats
  • Range: 8.000 m (8,749 yd)
  • Guidance:
    • Fire and forget
    • Capability in adverse weather and battlefield obscurants
    • Inertial guidance
    • Millimeter wave radar seeker
    • Home-on-jam anti-radiation mode
  • Warhead: 9 kg (20 lb) tandem shaped charge high explosive anti-tank (HEAT)
  • Length: 176 cm (69.2 in)
  • Weight: 49 kg (108 lb)

[edit] AGM-114M Hellfire II

  • Target: Bunkers, light vehicles, urban (soft) targets and caves
  • Range: 8.000 m (8,749 yd)
  • Guidance:
    • Semi-active laser homing
  • Warhead: Blast fragmentation/incendiary
  • Weight: 48 kg (105 lb)
  • Length: 163 cm (64 in)

[edit] AGM-114N Hellfire II

  • Target: Enclosures, ships, urban targets, air defense units
  • Range: 8.000 m (8,749 yd)
  • Guidance:
    • Semi-active laser homing
  • Warhead: Metal augmented charge (MAC)
  • Weight: 48 kg (105lb)
  • Length: 163 cm (64 in)

[edit] AGM-114P Hellfire II

  • Version of AGM-114K optimized for use from UAVs flying at high-altitude.

[edit] Rocket motor

Cross section diagram of Hellfire rocket motor, showing the rod and tube grain design.
Cross section diagram of Hellfire rocket motor, showing the rod and tube grain design.
  • Contractor: Alliant Techsystems
  • Designation:
    • M120E3 (Army)
    • M120E4 (Navy)
  • Main features:
    • Qualified minimum smoke propellant
    • Rod and tube grain design
    • Neoprene bondline system
  • Performance:
    • Operating temperature: −43 °C to 63 °C (−45 °F to 145 °F)
    • Storage temperature: −43 °C to 71 °C (−45 °F to 160 °F
    • Service life: 20+ years (estimated)
  • Technical data:
    • Weight: 14.2 kg (31.3 lb)
    • Length: 59.3 cm (23.35 in)
    • Diameter: 18 cm (7.0 in)
    • Case: 7075-T73 aluminum
    • Insulator: R-181 aramid fiber-filled EPDM
    • Nozzle: Cellulose phenolic
    • Propellant: Minimum smoke cross linked double based (XLDB)

[edit] Photos


[edit] See also

[edit] References

[edit] External links

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