• Home
  • Download PDF
  • Order CD-ROM
  • Order in Print
High-explosive fragmentation (HE-FRAG) warheads - 14024_71
GP WARHEAD - 14024_73

Aviation Ordinanceman 1 - Aviation theories and other practices
Page Navigation
  57    58    59    60    61  62  63    64    65    66    67  
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







Western Governors University

Privacy Statement
Press Release
Contact

© Copyright Integrated Publishing, Inc.. All Rights Reserved. Design by Strategico.