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Page Title: MISSILE LIQUID COOLING UTILITY SYSTEM
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WAVEGUIDE PRESSURIZATION SYSTEM
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Aviation Structural Mechanic E2 - How airplanes are built and how to maintain them
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SYSTEM  OPERATION

waveguide   pressure   during   an   overpressure condition. Air Desiccators The  waveguide  pressurization  system  contains two  air  desiccators.  The  desiccators  remove moisture  from  the  regulated  air.  The  desiccators contain desiccant to absorb moisture and a silica gel   for   an   indicating   agent.   During   normal operation, the silica gel is blue. When moisture saturation occurs, the gel turns pink. The color change is visible through an inspection window on the housing of the desiccator. Ground Test Ports The  waveguide  pressurization  system  contains two test ports, one for electronic countermeasures and one for the radar waveguide. The two test ports  provide  a  method  of  using  a  ground  air source to pressure test the system. MISSILE  LIQUID  COOLING UTILITY  SYSTEM Learning  Objective:  Identify  operating principles  and  maintenance  safety  pre- cautions for missile liquid cooling utility systems. The liquid cooling system in the F-14 aircraft is  used  with  both  the  radar  and  missile  systems. The  cooling  system  heats  and  cools  the  Phoenix missile. The temperature control system consists of a weapons control system (WCS) cooling loop for the radar system and a missile cooling loop for the missile system; both loops are controlled by a common controller. In each loop, a dielectric coolant  fluid  is  circulated  by  a  motor-driven pump.  The  fluid  is  filtered  to  remove  air, moisture, and foreign matter. The right Phoenix missile  fairing  (fig.  1-17)  contains  the  mis- sile  coolant  pump  assembly  and  the  missile Figure 1-17.—Missile fairing. 1-23

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