Chapter 3 UREs Flashcards
- (412) In addition to a ground maintenance reply (GMR) 25, what else will be reported to the LCC when the MGS reaches 80 degrees fahrenheit?
A. Launch facility no-go (LFNG)
*B. GROSS TEMP
C. Nothing else
D. NO-GO
- (412) About how many gallons of coolant does the tank of the guidance section liquid cooler store?
A. 2
*B. 7
C. 14
D. 20
- (413) Aside from the hydraulic lines, what is the last component in the guidance section liquid cooler the coolant flows through before entering the MGS?
A. Filter
B. Coolant tank
*C. Control valve
D. Coolant pump
- (413) A decrease in the thermistor resistance would indicate a
*A. temperature increase in the MGS.
B. “close valve” signal is being sent to the control valve.
C. ground maintenance reply (GMR) 25.
D. temperature decrease in the MGS.
- (413) During power applied check out, what action, if any, is required if the red NO-GO indicator on the electronic control amplifier illuminates?
*A. Shut down the MGS manually
B. No action required, the MGS will shutdown automatically
C. Shut down the G&C liquid cooler automatically
D. Manually set G&C temperature alarm switch on the PG to NORMAL position
- (414) What Minuteman system monitors missile functional performance,provides signals and ground power, maintains the liquid coolant,and the environmental control required to sustain missile operation until launch?
A. Aerospace vehicle equipment (AVE)
*B. Operational ground equipment (OGE)
C. Operational support equipment (OSE)
D. Maintenance support equipment (MSE)
- (414) Which of the following is the controller-monitor not required for aerospace vehicle equipment (AVE) startup?
A. Power signal distribution unit (PSDU) repair is accomplished.
B. G&C coupler drawer replacement
*C. RS maintenance is accomplished
D. MGS replacement
- (415) During the digital computer unit (DCU) memory loading, where is the program data contained before it is loaded into the DCU memory?
A. G&C coupler
*B. Magnetic tape cartridge (MTC)
C. MGS
D. Controller-monitor
- (415) Why are OGE and AVE startup normally not required during code change loading?
A. LF is in local control
*B. G&C system is already in strategic alert
C. MCC commanded remote missile startup
D. G&C does not require the OGE and AVE to started up
- (415) Digital computer unit (DCU) program loading requires the use of a cartridge tape unit (CTU), controller-monitor,
A. code change verifier (CCV), and LFLC.
*B. cable set, and LFLC.
C. and LFLC.
D. and CCV.
- (415) If an ERROR indicator-on-condition and output status of the CTU is parity error stop, which of the following will be unsuccessful?
A. Tape load
B. CTU self test
*C. Conditioning cycle
D. Tape track ID block readout
- (415) The tape ID block tells the operator that the tape cartridge is for a particular
A. wing.
B. flight.
C. squadron.
*D. LF
- (415) How does the CTU determine when the end-of-file is reached?
*A. A tape mark is detected
B. The early warning hole is detected
C. By a program within the tape cartridge
D. The load point for the next file is detected
- (415) The computer memory security check (CMSC) number consists of how many digits?
A. 4
B. 5
*C. 8
D. 12
- (415) When does the digital computer unit (DCU) exit into strategic alert?
A. Upon successful readout of the computer memory security check (CMSC) number
B. After operator initiates system into compute
*C. Completion of the alignment mode
D. When the master reset sets true