B2w051 Edition 7 Volume 3 Comprehensive Review

75 Questions | Total Attempts: 72

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Aircraft Quizzes & Trivia

B2W051 Edition 7 Volume 3 Comprehensive Review


Questions and Answers
  • 1. 
    Which type of guidance system tracking energy produces a beam of coherent highly directional and intense light?
    • A. 

      Electro-optical.

    • B. 

      Light energy.

    • C. 

      Inertial.

    • D. 

      Radar.

  • 2. 
    Which type of guidance system is also known as television guided?
    • A. 

      Electro-optical.

    • B. 

      Light energy.

    • C. 

      Inertial.

    • D. 

      Radar.

  • 3. 
    Which type of guidance system is nothing more than very high frequency radio waves?
    • A. 

      Electro-optical.

    • B. 

      Light energy.

    • C. 

      Inertial.

    • D. 

      Radar.

  • 4. 
    Which type of guidance system gives the pilot a greater stand-off distance?
    • A. 

      Radar.

    • B. 

      Laser.

    • C. 

      Electro-optical/television (TV).

    • D. 

      Global positioning system aided inertial navigation system (GAINS).

  • 5. 
    In which type of guidance system does the weapon send out the tracking energy?
    • A. 

      Active.

    • B. 

      Passive.

    • C. 

      Semi-active.

    • D. 

      Semi-passive.

  • 6. 
    Which type of precision-guided munitions (PGM) hones in on energy reflected off the target by another source?
    • A. 

      Active.

    • B. 

      Passive.

    • C. 

      Semi-active.

    • D. 

      Semi-passive.

  • 7. 
    What system is actually the brain of precision-guided munitions (PGM)?
    • A. 

      Control.

    • B. 

      Guidance.

    • C. 

      Armament.

    • D. 

      Propulsion.

  • 8. 
    The purpose of the fixed control surfaces used on guided munitions is to
    • A. 

      Provide ballast in flight.

    • B. 

      Stabilize the weapon in flight.

    • C. 

      Steer the weapon to the target.

    • D. 

      Provide aerodynamics in flight.

  • 9. 
    The purpose of the movable control surfaces used on guided munitions is to
    • A. 

      Provide ballast in flight.

    • B. 

      Stabilize the weapon in flight.

    • C. 

      Steer the weapon to the target.

    • D. 

      Provide aerodynamics in flight.

  • 10. 
    To move their control surfaces, precision guided munitions (PGM) use either hydraulic, pneumatic, or
    • A. 

      Electro-servo actuators.

    • B. 

      Proportional.

    • C. 

      Electronic circuits.

    • D. 

      Pressurized fluid.

  • 11. 
    A control system that can make minor or large corrections relative to the flight path of the target is said to have
    • A. 

      A “bang-bang” control system.

    • B. 

      A closed-loop control system.

    • C. 

      Proportional navigation.

    • D. 

      Directional navigation.

  • 12. 
    The air-to-air missile proximity fuze detonation occurs when
    • A. 

      A predetermined amount of time elapses.

    • B. 

      The missile senses the target getting closer.

    • C. 

      The missile senses the target moving farther away.

    • D. 

      The missile comes into direct contact with the target.

  • 13. 
    What type of rocket motor propellant is used in air-to-air missiles?
    • A. 

      Gas grain.

    • B. 

      Granular.

    • C. 

      Liquid.

    • D. 

      Solid.

  • 14. 
    Live missiles must always have a ground wire attached to them to prevent static electricity from
    • A. 

      Damaging the internal circuits.

    • B. 

      Igniting their rocket motors.

    • C. 

      Damaging the missile.

    • D. 

      Arming the fuze.

  • 15. 
    What components, minimum, make up a propulsion system?
    • A. 

      Rocket motor (RM), RM igniter, and nozzle.

    • B. 

      RM, propellant, and nozzle.

    • C. 

      Fuel and RM igniter.

    • D. 

      RM and RM igniter.

  • 16. 
    What warhead does the guided-bomb unit (GBU)–12 laser guided bomb (LGB) use?
    • A. 

      MK–82.

    • B. 

      MK–83.

    • C. 

      MK–84.

    • D. 

      BLU–109.

  • 17. 
    The MAU–169 series computer control group (CCG) consists of a detector,
    • A. 

      Computer unit, and warhead section.

    • B. 

      Computer, and control section.

    • C. 

      Igniter, and computer control section.

    • D. 

      Control section, and warhead.

  • 18. 
    Which guided-bomb unit (GBU) laser guided bomb (LGB) uses a 2,000 pound bombs?
    • A. 

      GBU–10.

    • B. 

      GBU–12.

    • C. 

      GBU–39.

    • D. 

      GBU–54.

  • 19. 
    What purpose does the WGU–12/WGU–39 series guidance control unit (GCU) seeker platform assembly serve?
    • A. 

      Send signals to the computer group which determines the direction to target.

    • B. 

      Connect the GCU to the warhead.

    • C. 

      “Look” for the reflected laser light signal.

    • D. 

      Hold the GCU seeker.

  • 20. 
    The purpose of the BSU–84 airfoil group (AFG) is to
    • A. 

      Provide aerodynamic lift and stability during flight.

    • B. 

      Create smooth and stable flight while in glide mode.

    • C. 

      Provide steering commands for the control surfaces.

    • D. 

      Steer the bomb and provides aerodynamic lift.

  • 21. 
    The purpose of the aft faring assembly used on the GBU–24A/B is to
    • A. 

      Provide an aerodynamic interface between the bomb and wing assembly.

    • B. 

      Extend the bomb charging well conduit to the hardback assembly.

    • C. 

      Provide more distance between the bomb and bomb rack.

    • D. 

      Provide the aerodynamic lift and stability during flight.

  • 22. 
    What work package (WP) contains procedures for testing a laser guided bomb (LGB) computer control group (CCG)?
    • A. 

      WP 070 00.

    • B. 

      WP 080 00.

    • C. 

      WP 090 00.

    • D. 

      WP 998 00.

  • 23. 
    What tester is the TTU–595 designed to replace for field testing all laser guided bomb (LGB) computer control groups (CCG)?
    • A. 

      Computer test set, AN/GJM–50.

    • B. 

      Digital test set, AN/GYQ–79.

    • C. 

      Digital test set, TTU–395.

    • D. 

      Digital test set, TTU–373.

  • 24. 
    The wing actuator tool used to perform what maintenance task?
    • A. 

      Install the forward adapter.

    • B. 

      Install and remove the wing.

    • C. 

      Deploy the wing in flight.

    • D. 

      Open and close the wings.

  • 25. 
    The typical Joint Direct Attack Munition (JDAM) tail assembly consists of a tail fairing/structure, tail actuator subsystem (TAS), wire harness assembly, guidance control unit (GCU),
    • A. 

      Global positioning system (GPS) antenna, two moveable control fins, and two fixed fins.

    • B. 

      GPS antenna, three moveable control fins, and one fixed fin.

    • C. 

      Three moveable control fins, and one fixed fin.

    • D. 

      And control fins.

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