Four dummy Hydra 70 rockets and an inert AGM-114 Hellfire
|Place of origin||United States|
|Used by||See Users|
|Weight||13.6 lb (6.2 kg) (Mk 66 Mod 4 rocket motor only) |
|Length||41.7 in (1,060 mm)|
|Diameter||2.75 in (70 mm)|
|Muzzle velocity||2,300 feet per second (700 m/s)|
|Effective range||8,700 yards (8,000 m)|
|Maximum range||11,500 yards (10,500 m)|
|Speed||2,425 ft/s (739 m/s)|
|AH-64 Apache, AH-1Z Viper, AH-1 Cobra, OH-58 Kiowa, Eurocopter Tiger, A-10 Thunderbolt II, UH-60 Black Hawk, P-3 Orion, MH-6 Little Bird, F-16 Fighting Falcon, AV-8B Harrier II|
The Hydra 70 family of WAFAR (Wrap-Around Fin Aerial Rocket), based on the Mk 66 universal motor, was developed from the previous 2.75 inch Mk 40 motor-based folding fin aerial rocket. The propellant grain is longer and of a different formulation than that of the MK40/MK4, however, the stabilizing rod and igniter are essentially the same design. The MK66 motors have a substantially higher thrust, 1,335 pounds-force (5,940 N) (Mod 2/3) 1,415 pounds-force (6,290 N) (Mod 4), and a longer range than the older motors. To provide additional stability the four rocket nozzles are scarfed at an angle to impart a slight spin to the rocket during flight. 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. Today, the OH-58D(R) Kiowa Warrior and AH-64D Apache Longbow, as well as the Marine Corp's AH-1 Cobra, carry the Hydra rocket launcher standard on its weapon pylons.
Mk 66 rocket motor variants
|Mk 66 Mod 0||70 mm (2.75 in) WAFAR universal motor; common motor for the GD Hydra 70 series of rockets; original prototype; for US Army|
|Mk 66 Mod 1||Mk 66 variant; production variant; for US Army|
|Mk 66 Mod 2||Mk 66 Mod 1 variant; HERO (Hazards of Electromagnetic Radiation to Ordnance) safe; for US Navy and US Air Force|
|Mk 66 Mod 3||Mk 66 Mod 1 variant; HERO safe; Mk 66 Mod 2 for US Army|
|Mk 66 Mod 4||Mk 66 Mod 2/3 variant; incorporates a Salt rod to reduce exhaust gases; for all services|
|Mk 66 Mod 5||Mk 66 Mod 4 variant; Incorporates propellant venting during fast cook off|
|Mk 66 Mod 6||Mk 66 Mod 4/5 variant; designed to reduce the tendency of secondary launch gasses to combust in the parent aircraft’s engine, primarily with the AH-64 helicopter|
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.
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 H-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.
Common U.S. Mk 66 compatible launchers
|M260||7-Tube LWL (LightWeight Launcher)|
|M261||19-Tube LWL (LightWeight Launcher)|
|LAU-130/A||19-Tube rocket launcher|
|LAU-131/A||7-Tube rocket launcher|
|LAU-68D/A||7-Tube LAU-68C/A variant; compatible w/ Mk 66 rocket motor; external thermal protection coating; launcher supports single and ripple firing|
|LAU-61C/A||19-Tube LAU-61B/A variant; compatible w/ Mk 66 rocket motor; external thermal protection coating; launcher supports single and ripple firing|
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.
|#||Designation||Description||Arming Range, Acceleration or Time|
|1||M423||Nose Mount, Point Detonating for slow speed platforms (helicopters)||47 to 102 yards (43 to 93 m)|
|2||M427||Nose Mount, Point Detonating for high speed platforms||197 to 466 yards (180 to 426 m)|
|3||XM436||Air burst, Motor-Burnout Delay|
|4||XM438/M438||Nose Mount, Point Detonating|
|6||Mk 352 Mod 0/1/2||Point Detonating|
|7||M429||Proximity Air burst|
|8||M433||Nose Mount, Resistance Capacitance (RC)||SuperQuick (PD) 11 to 49 yards (10 to 45 m) Delay in 5.5 yards (5.0 m) increments including 3.3 yards (3.0 m) Bunker penetrating option|
|9||M439||Base Mount, Resistance Capacitance (RC), Payload Discharging Pilot-Selectable||Discharges SMs between 547 and 7,874 yards (500 and 7,200 m) (766 to 7,546 yards [ 700 to 6,900 m ] on AH-1s) 27Gs|
|10||M442||Air burst, Motor-Burnout Delay||Discharges Flare at 3,281 yards (3,000 m), 17-22G required for arming|
|11||M446||Base Mount, Air burst, Motor-Burnout Delay|
|12||Model 113A||Base Mount, Air burst, Motor-Burnout Delay|
|Designation||Description||Weight||Payload||Fuze Type||Fuzing options|
|M151||High explosive (HEPD) '10 pounder'||8.7 pounds (3.9 kg) (w/o Fuze)||2.3 pounds (1.0 kg) Comp B-4 HE||M423||1,2,5,7,8|
|M156||White phosphorus (WP)||9.65 pounds (4.38 kg)||2.2 pounds (1.00 kg) WP||M423 M429||1,2,6,7|
|M229||High explosive (HEPD); elongated M151 '17 pounder'||17.0 pounds (7.7 kg) (Fuzed)||4.8 pounds (2.2 kg) Comp B-4 HE||M423||1,2,6,7|
|XM245||Submunition warhead possibly a modernized XM80/XM99||32 XM100 CS canisters||3|
|M247||High-explosive anti-tank (HEAT)/high-explosive dual purpose (HEDP)||8.8 pounds (4.0 kg)||2.0 pounds (0.91 kg) Comp B HE||M438 PD||4 (integral to warhead)|
|M255||APERS (anti-personnel) warhead||2500 28 grains (1.8 g) flechettes||9|
|M255E1/A1||Flechette warhead||14.0 pounds (6.4 kg)||1179 60 grains (3.9 g) flechettes||M439||9|
|M257||Parachute illumination||11.0 pounds (5.0 kg)||One M257 Candle (Flare) 1 million candela||M442||10 (integral to warhead)|
|M259||White phosphorus (WP)||9|
|M261||Multi-purpose submunition (MPSM)||13.5 pounds (6.1 kg)||9 M73 (Grenade) Submunitions||M439 with M84 electric detonator||9|
|M264||Red phosphorus (RP) Smoke||8.6 pounds (3.9 kg)||72 RP Pellets||M439||9|
|M267||MPSM Practice||13.5 pounds (6.1 kg)||Three Marking SMs, 6 Metal Weights||M439 with M84 electric Detonator||9|
|M274||Practice (Smoke)||9.3 pounds (4.2 kg)||2 ounces (57 g) of potassium perchlorate and aluminum powder||M423||1|
|M278||Infra-red (IR) parachute illumination||11.0 pounds (5.0 kg)||One M278 IR Flare||M442||10 (integral to warhead)|
|Mk 67 Mod 0||White phosphorus (WP)||1,2,6,7|
|Mk 67 Mod 1||Red phosphorus (RP)||1,2,6,7|
|WTU-1/B||Practice||9.3 pounds (4.2 kg)||Inert||None||None|
|WDU-4/A||APERS warhead||9.3 pounds (4.2 kg)||96 flechettes of unknown weight||12 (integral to warhead)|
|WDU-4A/A||APERS warhead||9.3 pounds (4.2 kg)||2205 20 grains (1.3 g) flechettes||12 (integral to warhead)|
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
The Advanced Precision Kill Weapon System (APKWS) II is a program to provide a laser guidance to the existing Hydra 70 systems in service. It was cancelled by the US Army in February 2007, but was restarted by the US Navy in 2008. Similar programs are the US Navy Low-Cost Guided Imaging Rocket, Lockheed Martin Direct Attack Guided Rocket and the ATK/Elbit Guided Advanced Tactical Rocket – Laser. APKWS has been fired successfully from the AH-64 Apache by BAE Systems in trials at Yuma Proving Grounds in early September, 2013; US Navy trials of the APKWS with the A-10 Thunderbolt II, the AV-8B Harrier and the F-16 Fighting Falcon led to US Central Command's approval of a modified version of APKWS to be fired from fast-moving jet aircraft.
- Philippines, The launchers are mounted on AS-211 "Warrior" trainers with secondary combat capability and 520MG Defender helicopters.
- United Arab Emirates
- United Kingdom
- United States
- South Korea
- Rockets galore
- Hydra-70 2.75-inch (70mm) family of rockets (PDF), General Dynamics Armament and Technical Products, 2012, p. 2.
- "Hydra 70", Munitions, Military, Global Security.
- Hydra 70 (PDF), GDATP.
- R&D Budget Request (PDF), US Army, 2008, p. 4.
- "Hydra 70". GlobalSecurity. Retrieved 2005-09-01.
- Hydra-70 Rockets: From Cutbacks to the Future of Warfare, Defense Industry Daily, 2006-4 .
- Air-Launched 2.75-Inch Rockets, Designation Systems.
- "Hydra-70", Warheads energetics, Weapon Systems, General Dynamics.
- 2012 Army Weapon Systems Handbook
- Hydra-70 Rocket System