Chapter 3 UREs Flashcards

0
Q
  1. (015) Which statement best describes the function of the PDU in the MGS?
A

A. Relays command signals to the missile flight control hardware.
B. Serves as a floating ground point within the MGS to improve system reliability.
*C. Isolates the loads between the MGS and flight controls through the use of a diode block.
D. Responsible for commanding missile battery activation and flight control ground power turn-off prior to launch.

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1
Q
  1. (015) Which statement best describes a function of the MGS?
A

*A. It is the primary element for missile guidance, navigation, and control.
B. It provides the LCC with in-flight data and telemtry
C. Its operational ground program (OGP) squibs the SRAM battery prior to launch.
D. It operates separately from the OGP/OFP, to guide and conclude missile flight and payload deployment.

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2
Q
  1. (015) Which battery in the MGS ensures MGC data integrity during power loss?
A

A. Flight battery
B. Flight control battery
*C. SRAM battery
D. Aerospace vehicle equipment (AVE) battery backup

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3
Q
  1. (015) Which MGS component contains electronics and provides power to accelerometers, gyroscopes, and torque motors?
A

A. Flight controller set (FCS)
B. Power distribution unit (PDU)
C. Missile guidance computer (MGC)
*D. Missile guidance set control (MGSC)

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4
Q
  1. (016) Which item is used to accomplish the operational certification of the NS-50 missile guidance set (MGS)?
A

A. 82 bench
B. Nuclear certification test station
*C. Missile guidance set test set (MGSTS)
D. Ground Minuteman automated test station (GMATS)

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5
Q
  1. (016) How does the MGSTS indicate that an excessive power condition exists?
A

A. Indicator lamp only
*B. Indicator lamp and aural alarm
C. Visual display unit indicates alarm code
D. Visual display unit indicates malfunction code

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6
Q
  1. (016) The virtual control processor simulates what MGS components during self-test of the MGSTS?
A

A. Flight controller and SRAM
B. Flight controller and RAM
*C. Missile guidance computer (MGC) and SRAM
D. Computer and flight controller

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7
Q
  1. (017) During the MGSTS SRAM battery test, the output of the power module is loaded by what?
A

A. Dummy load
B. Alarm test set
*C. Toggle switches
D. System program software

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8
Q
  1. (017) The MGSTS SRAM battery power safing test verifies proper operation of the
A

A. VXI module.
*B. limit detectors.
C. SRAM battery.
D. guidance set computer.

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9
Q
  1. (017) What test must be accomplished after completion of a Missile Guidance Set (MGS) certification?
A

A. GMATS self-test
B. R/S extender cable certification
*C. MGSTS self-test
D. Missile guidance set computer memory checks

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10
Q
  1. (018) How many equipment bays or racks does the ground Minuteman automated test station (GMATS) have?
A

A. 2
*B. 4
C. 6
D. 8

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11
Q
  1. (018) Which component is not one of the functional groups of the electronic equipment test station?
A

A. Computer
B. Instrumentation
C. Power and switching
*D. Interface test adapters

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12
Q
  1. (018) The computer group is made up of the
A

A. system controller, computer, and printer.
B. printer, system controller, and bar-code reader.
*C. bar-code reader, computer, and system controller.
D. mobile work surface, computer, and system controller.

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13
Q
  1. (018) Which component contains the pre-programmed instructions for testing a UUT?
A

A. Computer
B. Programmer
*C. System controller
D. Mobile work surface

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14
Q
  1. (018) How many power supplies make up the power and switching group?
A

A. 3
B. 6
C. 9
*D. 11

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15
Q
  1. (018) What is the purpose of the unit power controller (UPC)-3 in the power and switching group?
A

A. Controls cooling air to the power supplies.
B. Regulates data signals to the UUT.
*C. Controls the parameters of the AC power supply.
D. Provides EMI protection to the electronic test station.

16
Q
  1. (018) What is the purpose of the microcontroller?
A

A. Controls all circuit card functions of the test station.
B. Monitors power requirements needed for the mobile work station (MWS).
C. Reduces diagnostic time and increases accuracy of UUT testing.
*D. Prevents power from being sent through the interface carrier assembly (ICA) when no interface test adapter (ITA) is present.

17
Q
  1. (018) What allows the instrumentation group to interface with the computer group?
A

A. Tracewell chassis
B. Power distribution unit
C. High-speed serial interface bus
*D. High-speed parallel interface bus and three Hewlett-Packard interface buses (HP-IB)

18
Q
  1. (018) Which component of the test station performs measurements within a specified sweep time?
A

A. RF power meter
B. Function generator
*C. Spectrum analyzer
D. Microcontroller

19
Q
  1. (018) Which is not a function of the universal counter?
A

A. Measuring the time interval and relative phase between two independent signals.
*B. Taking voltage and resistance measurements on a UUT.
C. Performing frequency measurements of RF signals.
D. Measuring the pulse width of a signal on one channel.

20
Q
  1. (018) what is the purpose of the mobile work surface (MWS)?
A

*A. Contains a support structure on which to mount and provide cooling air to the UUT.
B. Used as a platform for the monitor and keyboard of the test station.
C. To contain power supplies and other test equipment.
D. To provide input power and stimuli for the UUT.