The Hydra 70rocket is an American made 2.75-inch (70 mm) diameter 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 CRV7, with which it is physically interchangeable.
Overview
The Hydra 70 is derived from the 2.75-inch (70 mm) diameter 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 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 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-64E Apache Longbow, as well as the Marine Corps' versatile UH-1 Huey and AH-1 Cobra, carry the Hydra rocket launcher standard on its weapon pylons.[3]
Mk 66 rocket motor variants
Designation
Description
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 gases to combust in the parent aircraft’s engine, primarily with the AH-64 helicopter
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-64 Apache and AH-64D Apache Longbow helicopter variants 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-1W SuperCobra and 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.
7-Tube LAU-68C/A variant; compatible w/ Mk 66 rocket motor; external thermal protection coating; launcher supports single and ripple firing
LAU-69D/A
19-Tube LAU-61B/A variant; compatible w/ Mk 66 rocket motor; external thermal protection coating; launcher supports single and ripple firing
Accidents
In 2019, a 72-year-old Taiwanese man was killed after a discarded Hydra rocket which he had cut into with an electric saw exploded. He had believed it to be a length of pipe. The rocket had been caught in the net of a fishing vessel and then discarded by the crew ashore as scrap metal.[4]
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 settable fuzes using the "wall-in-space" concept or fixed standoff fuzes.
Training warheads.
Fuzing options
#
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
5
M440
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 submunitions 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), 17-22 g required for arming
11
M446
Base Mount, Air burst, Motor-Burnout Delay
12
Model 113A
Base Mount, Air burst, Motor-Burnout Delay
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.[5] The M247 HEDP warheads have similar penetration to the standard M72 LAW warhead (~300 mm of rolled homogenous armor).[6]
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 APKWS was the first to be fielded in March 2012,[9] and the TALON entered full rate production for the United Arab Emirates Armed Forces in September 2014.[10]
The Turkish ROKETSANCirit is a similar missile compatible with 70 mm rocket launchers, but it was developed from scratch and doesn't use Hydra 70 components.[11]
^ abHydra-70 2.75-inch (70mm) family of rockets(PDF), General Dynamics Armament and Technical Products, 2012, p. 2, archived from the original on 3 December 2012, retrieved 1 November 2012.
^ abcdeHydra 70(PDF), GDATP, archived from the original on 4 July 2010, retrieved 6 August 2010.
^Stipanović, Željko; Karačić, Marinko (October 2018). "Kiowa Warrior - Live Firing and Rocket Launching"(PDF). CROMIL – Croatian Military Magazine. No. 18. Croatian Ministry of Defence. pp. 18–19. Archived from the original(Magazine) on 29 December 2021. Retrieved 31 January 2024.