TX-59 HAWK
Motor | MIM-23 HAWK | |
Length | 108 inches | 16 feet 8 inches |
Diameter | 14 inches | 14 inches |
Weight | 849 lbs. | 1288 lbs |
Burn Time | 4.5 sec, boost 31 sec, sustain |
|
Maximum Thrust | 15,000 lbs, boost 1900 lbs sustain |
Developed in the mid-1950s for the U.S. Army, HAWK uses a two-level-thrust motor incorporating a dual-chamber design. Gas from the sustain phase burn exhausts out a tube running through the boost-phase chamber. Both phases exhaust out nozzle extension tubes that bypass the guidance equipment installed at the aft end of the missile. The TX-59, used for early HAWK development flights, is believed to be the first dual-chamber-design motor.
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