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THERMAL  JET  PROPULSION  SYSTEM
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Aviation Ordinanceman 2 & 3 - Aviation theories and other practices
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SERVICE GUIDED MISSILES

A1. A2. A3. A4. A5. A6. A7. A8. Figure 3-6.—AIM-7F/M Sparrow missile. REVIEW NUMBER 2 ANSWERS TO QUESTIONS Q1. THROUGH Q8. Guidance,  control,  armament,  and  propulsion are the major sections of guided missiles. The guidance  section is considered the brains of the missile. The three types of homing systems are  active,  semiactive,  and  passive  homing. If a missile gets its target illumination from the launching aircraft,  it as semiactive homing. The armament section consists of  the  payload,  fuzing,  safety  and  arming  (S&A) devices, and target-detecting devices (TDDs). Safety and arming devices maintain the explosive train of a fuzing system in a safe condition until the acceleration requirement is met after launch. The  two  types  of  propulsion  used  with  guided  missiles  are  atmospheric  (air breathing) jet and thermal jet. The atmosphere jet depends on the atmosphere to supply the oxygen for proper fuel  burning,  and  the  thermal  jet  contains  its  own  supply  of  oxygen  and  is independent from the atmosphere. 3-8

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