One shops CDC practise test. Not to sure of #91. Also, if any andswers are off. Please tell me. Thanks
Z-axis modulation.
Intensity modulation
Deflection modulation
Amplitude modulation
Azimuth only
Elevation only
Range and azimuth
Elevation and range
A-scan.
B-scan.
Raster scans.
Plan-position indicator scan
1
2
3
4
Data processing circuits.
Deflection circuits.
Video Circuits.
Cathode-ray tube
Deflection circuits.
Video circuits
Power Supply.
Cathode-ray tube
Deflection circuits
Video circuits
Power supply
CRT
Current through the two deflection plates.
Triggers to the two deflection plates
Current through the deflection coil
Triggers to the deflection coil
Prevents implosion if the CRT is broken
Keeps the phosphor coating from burning
Eliminates static charges on the deflection plates
Prevents collision between electrons in the beam and air molecules
0.45 µsec
3 µsec
5 µsec
8 µsec
1030 MHz
1070 MHz
1090 MHz
1270 MHz
A4, A1, B4, C2, D1.
C4, B3, B1, A4, D2
D4, B1, C2, D4, A1
B4, B1, C2, D4, A1.
A Mode 4 reply is being received
The aircraft is a pilotless drone or missile
The aircraft is declaring a military emergency
It is requested by the radar operator to identify the aircraft position
Communication failure.
Military emergency.
Engine failure
Hijacking
Interrogators and associated components
Radar transmitter VZWR
Radar jamming strength
Radar receivers
115 VAC
120 VAC
130 VAC
115 VAC or 230 VAC
Electronic attack (EA), suppression of enemy air defenses (SEAD), and electronic warfare (EW).
Electronic attack, suppression of enemy air defenses (SEAD), signal intelligence (SIGNT).
Command, control, and communication countermeasures (C³CM), suppression of enemy air defenses (SEAD), and electronic warfare (EW).
Command, control, and communication countermeasures (C³CM), suppression of enemy air defenses (SEAD), signal intelligence (SIGNT).
Electronic warfare support (ES), electronic attack (EA), and electronic protection (EP).
Suppression of enemy air defenses (SEAD), Electronic warfare support (ES), electronic attack (EA).
Suppression of enemy air defenses (SEAD), Electronic warfare support (ES), and electronic protection (EP)
Electronic warfare support (ES), electronic attack (EA), Command, control, and communication countermeasures (C³CM).
To exploit signal environment before an engagement
To provide a tactically oriented immediate response
To provide indirect support to theater commanders
To support long term intelligence
Prevent jamming from accruing
Identify all possible interferences
Isolate friendly from enemy forces
Integrate with other operational forces
Troposheric scatter and burn through range.
Atmospheric attenuation and tropospheric scatter
Victim radar characteristic and burn through range
Atmospheric attenuation and victim radar characteristics.
Confusion jammers, spot jammers, and sweep jammers
Spot jammers, sweep jammers, and barrage jammers
Deception jammers, confusion jammers, and spot jammers
Deception jammers, confusion jammers, and barrage jammers
An expendable aircraft-like vehicle used to provide deception
An expendable aircraft-like vehicle used to gather information
A manned aircraft flown in a different sector to mislead operators
A manned aircraft flown at different altitudes to mislead operators
Staggered PRF
Coded Pulse Anti-Clutter System
Manual gain control
Frequency agility
Fast time constant (FTC)
Manual gain control (MGC).
Moving target indicator (MTI)
Instantaneous automatic gain control (IAGC)
Pulse recurraence frequency
Transmitted pulse width
Pulse recurrence time
Antenna beam width
Pulse recurrence frequency
Transmitted pulse width
Pulse recurrence
Antenna beam width
15 degrees
20 degrees
25 degrees
30 degrees
Minimum approach range
Maximum approach range
Minimum instrument flight rule (IFR) altitude for the base.
Maximum instrument flight rule (IFR) altitude for the base
1000
3000
5000
6000
Moving target indicator reflector
Center-line reflector
Reference reflector
Bracket reflector
Weather returns
Large target fluctuations only
Large target fluctuations and weather returns
Large target fluctuations and provide target enhancement
Unipolar video
Bipolar video
Canceled unipolar video
Canceled bipolar video
Target data computer (TDC)
Signal data computer (SDC)
Computer data entry module (CDEM)
Antenna beam position control (ABPCU)
24
37
74
137
3
4
5
6
Every PRT
Once every 2 seconds
Once per track interval
At beam interrupt signal time
Command, input, and output
Command, open-loop, closed-loop
Diagnostic, operational, coherent
Data point, closed-loop, self-test
One’s component
Repeater logic
Closed-loop
Open-loop
Safety zone
Elevation angle
Distance to taxiway
Distance to touchdown
Azimuth and range
Range only
Range and elevation
Elevation only
.5 microseconds
1
1.3
1.5
15 cycle rate
30
60
120
37-mhz crystal oscillator
74-mhz crystal oscillator
Local oscillator
Stable local oscillator
120 mhz
74
37
24
L-band
S-band
W-band
X-band
.5 microsecond
1
1.35
1.53
Provide voltage amplification and trigger shaping for the TWAT
Modulate the incoming video for conversion to IF
Produce excitation voltage for the cathode if the TWAT
Provide pulse shaping fit stable master oscillator
Traveling wave amplifier tube (TWAT) arc
High voltage (HV) deck fault
Standby converter fault
Airflow
Generate timing signal for the radar system
Provide predicted target location
Generate ultra high frequency (UHF) transmitter drive frequencies
Generate phase delay command to phase shifter elements of the antenna
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