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High-explosive fragmentation (HE-FRAG) warheads
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Aviation Ordinanceman 1 - Aviation theories and other practices
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GP WARHEAD

used against personnel and light material targets, such as trucks and parked aircraft. Upon detonation, a large quantity of metal fragments accelerate to a high velocity. This  action  damages  the  target.  The  types  of  HE-FRAG warheads currently in use are listed in table 2-1. HEAT WARHEADS.— High-explosive antitank (HEAT) warheads (fig. 2-13) are used against armored targets, such as tanks, bunkers, and armored vehicles. The   warhead   contains   a   shaped-charge.   When detonated,  it  produces  a  high-energy  jet  that  penetrates armored targets. The only HEAT warhead currently in use is the Mk 5 Mod 0. AT/APERS  WARHEAD.—  The  high-explosive antitank/antipersonnel   (AT/APERS)   warhead   (fig. 2-14)  combines  the  effectiveness  of  the  HE-FRAG  and HEAT  warheads.  The  explosive  shaped-charge  in  the AT/APERS  warhead  detonates  at  the  aft  end,  producing A1. A2. A3. A4. A5. A6. A7. A8. A9. A10. A11. A12. Table 2-1.—Service Warheads REVIEW NUMBER 1 ANSWERS TO QUESTIONS Q1. THROUGH Q12. The two rockets currently used by the Navy are the  2.75-inch  Mighty  Mouse  and the 5.0-inch Zuni. If a rocket does not fire when the firing circuit is energized, it is known as a  misfire. Thrust is the force exerted by the gases produced by the burning of the rocket motor  propellant. In rocket propulsion, the Venturi nozzle decreases turbulence of escaping gases and increases thrust. Gas pressure inside the container provides about  70% of the  force, and the escaping gases provide about  30% of the force to move the container  forward. The three components of a rocket are the  motor,  warhead,  and  fuze. The  components  of  rocket  motors  include  the  motor  tube,  propellant,  inhibitors, stabilizing rod, igniter and nozzle and fin assembly. The inhibitor  restricts or controls burning on the propellant. The  stabilizing   rod  is  salt  coated  to  prevent  unstable  burning  of  the  rocket propellant. Rockets are most susceptible to radio-frequency (RF) energy  when they aren't installed in the launcher, The scarfed nozzle installed in the Mk 40 rocket motor The Mk 16 rocket motor has  a modified igniter nozzle, and fin assembly. You should remove the fin retainer band on the Mk 71 rocket motor  when the rocket is installed into the launcher tube. 2-10

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