Trisha Shetty (Editor)

Hydra 70

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Type
  
Rocket

In service
  
1948–present

Unit cost
  
$2,799

Place of origin
  
United States

Used by
  
See Users

Hydra 70

Weight
  
13.6 lb (6.2 kg) (Mk 66 Mod 4 rocket motor only)

The Hydra 70 rocket is a 2.75-inch fin-stabilized unguided rocket used primarily in the air-to-ground role. It can be equipped with a variety of warheads, and in more recent versions, guidance systems for point attacks. The Hydra is widely used by US and allied forces, competing with the Canadian CRV-7 which is physically interchangeable.

Contents

Overview

The Hydra 70 is derived from the 2.75-inch Mk 4/Mk 40 Folding-Fin Aerial Rocket developed by the United States Navy for use as a free-flight aerial rocket in the late 1940s. The Mk 40 was used during the Korean and Vietnam wars, being used to provide close air support to ground forces from about 20 different firing platforms, both fixed-wing and armed helicopters.

The main change made to produce the Hydra was the Mk. 66 motor which uses a new propellant that offers considerably more thrust, 1,335 pounds-force (5,940 N) (Mod 2/3) 1,415 pounds-force (6,290 N) (Mod 4). The fins of the Mk 40 flipped forward from the rear when the rocket left the launching tube, but in the Hydra they are curved to match the outside diameter of the rocket fuselage and flip sideways to open, which is referred to as WAFAR (Wrap-Around Fin Aerial Rocket) instead of FFAR (folding-fin aerial rocket). To improve stability during the time while the fins are still opening, the four motor nozzles have a slight cant angle to impart a spin while the rocket is still in the launch tube.

Today, the OH-58D(R) Kiowa Warrior and AH-64D Apache Longbow, as well as the Marine Corps' AH-1 Cobra, carry the Hydra rocket launcher standard on its weapon pylons.

Service

The family of Hydra 70 (70 mm) 2.75 inch rockets perform a variety of functions. The war reserve unitary and cargo warheads are used for anti-materiel, anti-personnel, and suppression missions. The Hydra 70 family of folding-fin aerial rockets also includes smoke screening, illumination, and training warheads. Hydra 70 rockets are known mainly by either their warhead type or by the rocket motor designation, Mk 66 in US military service.

United States

In the U.S. Army, Hydra 70 rockets are fired from the AH-64A Apache and AH-64D Apache Longbow helicopters using M261 19-tube rocket launchers, and the OH-58D Kiowa Warrior using seven-tube M260 rocket launchers. In the U.S. Marine Corps, either the M260 or M261 launchers are employed on the AH-1 Cobra and future AH-1Z Viper, depending upon the mission. The M260 and M261 are used with the Mk 66 series of rocket motor, which replaced the Mk 40 series. The Mk 66 has a reduced system weight and provides a remote fuze setting interface. Hydra 70s have also been fired from UH-60 and AH-6 series aircraft in US Army service.

The AH-1G Cobra and the UH-1B "Huey" used a variety of launchers including the M158 seven-tube and M200 19-tube rocket launchers designed for the Mk 40 rocket motor; however, these models have been replaced by upgraded variants in the U.S. Marine Corps because they were not compatible with the Mk 66 rocket motor. The Hydra 70 rocket system is also used by the U.S. Navy, and the U.S. Air Force.

Warheads

Hydra 70 warheads fall into three categories:

  • Unitary warheads with impact-detonating fuzes or remote-set multi-option fuzes.
  • Cargo warheads with air burst-range, with setable fuzes using the "wall-in-space" concept or fixed standoff fuzes.
  • Training warheads.
  • Common warheads

    The most common warhead for the Hydra 70 rocket is the M151 "10-Pounder," which has a blast radius of 10 meters and lethal fragmentation radius of around 50 meters.

    NOTE: Though some of the warheads described were designed for the older Mk 40 rocket motor, but most likely could work with the Mk 66 motor if upgraded or modernized models were not available. However, this would not be necessary, as vast quantities of upgraded models exist today.

    Mk 66 rocket motor technical data

    Weight: 13.6 pounds (6.2 kg)

    Length: 41.7 inches (1,060 mm)

    Burn time: 1.05–1.10 sec

    Average thrust (77 F):

  • 1,335 lb (Mod 2/3)
  • 1,415 lb (Mod 4)
  • Motor burnout range: 1,300 feet (400 m)

    Motor burnout velocity: 2,425 ft/s (739 m/s)

    Launch spin rate: 10 rps, 35 rps after exiting launcher

    Velocity at launcher exit: 148 ft/s (45 m/s)

    Acceleration:

  • 60–70 g (initial)
  • 95–100 g (final)
  • Effective Range: 547 to 8,749 yards (500 to 8,000 m) depending on warhead and launch platform

    Maximum Range: 11,483 yards (10,500 m) under optimum conditions

    Precision guided Hydra 70

    There are several design efforts to turn the Hydra 70 rocket into a precision guided munition (PGM) to produce a weapon with greater accuracy but at less cost than other guided missiles. These include:

  • The BAE Systems Advanced Precision Kill Weapon System (APKWS) II
  • U.S. Navy Low-Cost Guided Imaging Rocket (LOGIR)
  • Lockheed Martin Direct Attack Guided Rocket (DAGR)
  • The ATK/Elbit Guided Advanced Tactical Rocket – Laser (GATR-L)
  • Raytheon TALON
  • Thales Group Roquette à Précision Métrique (RPM).
  • Forges de Zeebrugge SAL-Laser Guided Rocket (FZ275 LGR)
  • The APKWS was the first to be fielded in March 2012, and the TALON entered full rate production for the United Arab Emirates Armed Forces in September 2014.

    Roketsan Cirit is a similar missile compatible with 70 mm rocket launchers, but it was developed from scratch and doesn't use Hydra 70 components.

    Current operators

  •  Australia
  •  Croatia
  •  Egypt
  •  Iraq
  •  Kuwait
  •  Pakistan
  •  Philippines, The launchers are mounted on AS-211 "Warrior" trainers with secondary combat capability, SF-260 light attack aircraft and 520MG Defender helicopters.
  •  Saudi Arabia
  •  Singapore
  •  South Korea
  •  Thailand
  •  United Arab Emirates
  • References

    Hydra 70 Wikipedia