SURFACE TO AIR MISSILES (SAM)

I-HAWK

 

Launch of a Greek I-HAWK surface-to-air missile

Improved HAWK or I-HAWK - The original HAWK system had problems engaging targets at low altitude - the missile would have problems picking the target out against ground clutter.

 

 

 

The US army began a program to address these issues in 1964 - the HAWK Improvement Program (HAWK/HIP).

 

 

 

This involved numerous upgrades to the Hawk system:

  • A digital data processing central information coordinator for target processing, threat ordering, and intercept evaluation.

  • An improved missile (MIM-23B) with a larger warhead, smaller and more powerful M112 motor, and improved guidance section.

  • The PAR, CWAR, HPI, and ROR were replaced by upgraded variants

The I-HAWK has a larger 74 kg (163 lb) blast-fragmentation warhead, a smaller and improved guidance package, and a new M112 rocket motor. The new warhead produces approximately 14,000 two gram fragments that cover a much larger 70 degree arc. The missiles M112 rocket motor has a boost phase of 5 seconds and a sustain phase of 21 seconds. The motor's total weight is 395 kg including 295 kg of propellant. This new motor improves the engagement envelope to 1.5 km to 40 km in range at high altitude, and 2.5 km to 20 km at low altitude, the minimum engagement altitude is 60 m. The missile was operational in 1971. All US units had converted to this standard by 1978.
 

I-HAWK Specifications
Type Medium range surface-to-air missile
Manufacturer Raytheon
Weight 1,400lb (635kg)
Warhead 74kg blast fragmentation
Length 16ft 6in (5m)
Diameter 14.5in (3.8cm)
Wingspan 4 ft (1.2m)
Performance Speed Mach 2.5, range 25 miles, 40km), guidance semi-active radar, The original HAWK system had problems engaging targets at low altitude the I-Hawk additions include a digital data processing central information coordinator for target processing and uprated guidance system