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Page Title: Figure 2-5.—Mk 71 Mods motor, nozzle, and fin assembly
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Figure 2-4.—Mk 71 Mods motor, nozzle, and fin assembly
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Aviation Ordinanceman - Aviation theories and other practices
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HE-FRAG WARHEADS

the  2.75-inch  diameter  of  the  rocket.  The  fins  are notched at the tips to allow attachment of a fin retainer. The fin-actuating mechanism is a steel cylinder and a piston with a crosshead attached to its aft end. When the rocket is fired, gas pressure from the motor operates the  piston,  cylinder,  and  crosshead.  The  crosshead  is pushed against the heels of the fins, causing the fins to rotate on the fin pivot pins to the open position after the rocket leaves the launcher. After the fins have opened to the final flight position, the crosshead prevents the fins from closing. There are four nozzle inserts and the detent groove in the aft end of the nozzle plate. They hold the rocket in position after it is loaded in the launcher. The Mk 71 Mods motor has a modified igniter and a modified nozzle and fin assembly. The nozzle and fin assembly    (fig.    2-4)    contains    four,    spring-loaded, wraparound  fins  inside  the  motor  diameter.  The  steel nozzle expansion cone has flutes that cause the rocket to spin during free flight. This permits the rocket to be launched   from   high-speed   aircraft,   helicopters,   and low-speed aircraft. The   Mk   71   Mods   spring-loaded   fins   (fig.   2-5) deploy  after  emerging  from  the  rocket  launcher  tube. They lock in place (open) by sliding into a locking slot in the flange at the aft end of the fin nozzle assembly. When not actually installed in the launcher, the fins are held in the closed position by a fin retainer band, which must be removed when the rocket is installed into the launcher tube. The fin retainer band is not interchangeable with the shielding band. REVIEW NUMBER 1 Q1. List  the  two  rockets  currently  used  by  the Navy. Q2. If a rocket does not fire when the firing circuit is energized, it is known as a _____________. Q3. What is meant by the rockets thrust? Q4. In   rocket   propulsion,   the   Venturi   nozzle decreases  turbulence  of  escaping  gases  and increases   thrust.   Gas   pressure   inside   the container  provides  about  _______,  and  the escaping gases provide about __________ to move the container forward. Q5. List the three components of a rocket. Q6. List the components of rocket motors. Q7. What is the purpose of the inhibitor? Q8. What   rocket   component   is   salt   coated   to prevent    unstable    burning    of    the    rocket propellant? Q9. When should you remove the fin retainer band on a Mk 71 rocket motor? Warheads Different  tactical  requirements  demand  different types of rocket warheads be used with airborne rockets. 2-5 Figure 2-5.—Mk 71 Mods motor, nozzle, and fin assembly.

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