EOR For ground radar 3D135
The speed of light
The speed of sound
One-half the speed of light
One-half the speed of sound
A. 45.
b. 90.
C. 135.
D. 180
A. 3.09 ƒÝs.
B. 6.18 ƒÝs.
C. 9.27 ƒÝs.
D. 12.36 ƒÝs.
A. transmitter on-time.
B. transmitter off-time.
C. pulse recurrence time.
D. pulse repetition frequency.
A. A lower frequency than the original broadcast.
B. A higher frequency than the original broadcast.
C. No apparent frequency change than the original broadcastb||Œ
D. Oscillating lower and higher frequency changes in respect to the original broadcast._
A. Synchronizer.
B. Transmitter..
C. Modulator.r..
D. Duplexer..r..
A. Synchronizer.
B. Transmitter..
C. Modulator.r..
D. Duplexerr.r..
A. it is nonlinear.
B. it transmits patterns.ency.
C. it contains ferrite devices.
D. its transmit and receive patterns are identical.
A. Active
B. Linear
C. Passive
D. Circular
A. raise the effective beam coverage by 3.
B. dummy load the lower 3„a of the transmitted beam.LT
C. route the received signal from the number one feedhorn to a dummy load.b
D. vary low-level coverage by routing more radio frequency through one feedhorn.
A. Main lobe gain.
B. Pattern of the antenna.ices.
C. Probability of interference.
D. Susceptibility of the antenna.
A. gain.
B. location
C. purpose
D. power
A. direction of energy into an appropriately shaped beam
B. orientation of the electromagnetic wave as it travels through space.
C. motion of the antenna axis (of the beam) as the radar looks for an aircraftˆÊ
D. efficient launch and reception of electromagnetic energy in the atmosphere or space
A. Raster
B. Conical
C. Circular
D. Monopulse
A. Raster
B. Conical
C. Circular
D. Monopulse
A. Raster
B. Conical
C. Circular
D. Monopulse
A. Raster
B. Conical
C. Circular
D. Monopulse
A. Palmer
B. Helical
C. Palmer/Raster
D. Track-While
A. Simultaneous reception of pulse-type information
B. Near-simultaneous reception of pulse-type information
C. Electromagnetic (EM) waves reach the receiving antenna by direct paths
D. EM waves reach the receiving antenna by indirect paths
A. off-axis tracking.
B. frequency agility.
C. monopulse radar.
D. off-boresight tracking
A. Long-range surveillance
B. Airport surveillance.
C. Precision approach
D. Weather
A. Azimuth only.
B. Elevation only
C. Range and azimuth
D. Elevation and range
A. 1
B. 2
C. 3
D. 4
A. Data processing circuits
B. Deflection circuits..
C. Cathode-ray tube
D. Video circuits.
A. Deflection circuits..
B. Cathode-ray tube
C. Video circuits.
D. Power supply.
A. prevents implosion if the CRT is broken.
B. keeps the phosphor coating from burning.
C. eliminates static charges on the deflection plates.
D. prevents collisions between electrons in the beam and air molecules
A. 1030 MHz
B. 1070 MHz
C. 1090 MHz
D. 1270 MHz
A. a Mode 4 reply is being received.
B. the aircraft is a pilotless drone or missile.
C. the aircraft is declaring a military emergency
D. it is requested by the radar operator to identify the aircraft position.
A. Communication failure
B. Military emergency.
C. Engine failure.
D. Hijacking
A. Interrogators and associated components.
B. Radar antenna orientationce.
C. Radar jamming strengthionce.
D. Radar receivers
A. 115 Vac
B. 120 Vac
C. 230 vac
D. 115 Vac or 230 Vac
A. Spectrum conservation
B. Channel allocation
C. Ease of radiation
D. Companding
A. Amplitude of the modulating signal
B. Frequency of the modulating signal
C. Amplitude of the carrier signal
D. Frequency of the carrier signal
A. One-quarter of the modulating bandwidth
B. Four times the modulating bandwidth.i
C. Twice the modulating bandwidth.
D. Half the modulating bandwidth
A. inversely proportional to the amplitude of the modulating signal.s
B. directly proportional to the amplitude of the modulating signal.
C. inversely proportional to the phase of the modulating signal.
D. directly proportional to the phase of the modulating signal.
A. 5
B. 0.5
C. 0.3
D. 3
A. phase shifts at the rate of the modulating signal.
B. phase shifts with the phase of the modulating signal
C. amplitude shifts at the rate of the modulating signal
D. amplitude shifts with the phase of the modulating signal
A. two
B. three
C. four
D. five
A. 2 bit
B. 3 bit
C. 4 bit
D. 5 bit
A. Sampling
B. Rectifying
C. Oscillating
D. Band Limiting
A. 11 to 7 bits.
B. 11 to 8 bits.
C. 16 to 7 bits.
D. 16 to 8 bits.
A. By the receiving device to verify that the transmission was received correctly.
B. By the transmitting device to verify that the transmission was transmitted correctly.
C. By the modulator device to verify that the intelligence signal was received correctly
D. By the band limiting device to verify that the output signal was transmitted correctly
A. Communicates in parallel format.
B. Blocks many characters together for transmission
C. Eliminates the control bits, so more message data can be sent.
D. Uses low cost equipment to support synchronous transmission.
A. Determines parity.
B. Determines transmission rate.
C. Determines whether transmission is in ASCII format
D. Determines whether transmission is synchronous or asynchronous
A. The checksum.
B. Block check character.
C. The ASCII character set.
D. The sum of transmitted bits.
A. Checksum and cyclic redundancy check.
B. Longitudinal redundancy check and checksum.
C. Cyclic redundancy check and vertical redundancy check.
D. Vertical redundancy check and longitudinal redundancy check.
A. Checksum.
B. Cyclic redundancy.
C. Vertical redundancy.
D. Longitudinal redundancy.
A. Receiving end.
B. In the oscillator.
C. Transmitting end
D. In the primary buffers
A. The easy tap-ability of fiber optic cables reduces security risks.®x
B. Fiber optic cable has a higher attenuation than coaxial cable
C. Electromagnetic fields do not affect fiber optic cables.
D. Nuclear radiation does not affect fiber optic cable.
A. Easy to encrypt data.
B. Low signal attenuation.
C. Virtually impossible to tap a fiber optic cable unnoticed.Nã
D. Fiber optic cables are considerably smaller than metallic cable
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