MIM-23 Hawk - Missiles

Missiles

Type of Missile Entered
service
Tactical
model
Training and
Evaluation model
Prototype 1957 XM3
(XMIM-23A)
n/a
Basic Hawk 1959 (M3)
MIM-23A
XM16/18
(XMTM-23B/C)
Basic I-Hawk 1971
to
1978
MIM-23B XMEM-23B
Improved ECCM 1982 MIM-23C/D MEM-23C
Low-level/
multi-jamming
1990 MIM-23E/F MEM-23D
New body
section
early
1990s
MIM-23G/H MEM-23E
New warhead
and
fuzing (anti-TBM)
1995 MIM-23K/J MEM-23F
New fuzing only,
old warhead
1995 MIM-23L/M

The Hawk missile has a slender cylindrical body and four long chord clipped delta-wings, extending from mid-body to the slightly tapered boat-tail. Each wing has a trailing-edge control surface.

  • The MIM-23A is 5.08 metres (16.7 ft) long, has a body diameter of 0.37 metres (1 ft 3 in), a wing span of 1.21 metres (4 ft 0 in) and weighs 584 kilograms (1,290 lb) at launch with a 54 kilograms (120 lb) HE blast/fragmentation warhead. It has a minimum engagement range of 2 kilometres (1.2 mi), a maximum range of 25 kilometres (16 mi), a minimum engagement altitude of 60 metres (200 ft) and a maximum engagement altitude of 11,000 metres (36,000 ft).
  • The MIM-23B to M versions are 5.03 m (16.5 ft) long, have a body diameter of 0.37 m (1 ft 3 in) and, with a larger warhead of 75 kg (11 lb), weighing 638 kg (1,410 lb) at launch. An improved motor, with a total weight of 395 kg (870 lb) including 295 kg (650 lb) of propellant, increases the maximum range of the MIM-23B to M versions to 35 km (22 mi) and maximum engagement altitude to 18,000 m (59,000 ft). The minimum range is reduced to 1.5 km (0.93 mi). The MIM-23B has a peak velocity of around 500 m/s (1,600 ft/s). The missile is fitted with both radio frequency proximity and impact fuses. The guidance system uses an X-band CW monopulse semi-active radar seeker. The missile can maneuver at 15 g.

In the 1970s, NASA used surplus Hawk missiles to create the Nike Hawk sounding rocket.

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