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ECE : Satellite Communication - Quiz(MCQ)
A)
C
B)
X
C)
MF
D)
Ku

Correct Answer :   MF


Explanation : MF is a lower frequency band than Ku, C and X bands and does not lie in the microwave spectrum. Microwaves are used for satellite communication since the lower bands get reflected by the ionosphere.

A)
12Mpbs
B)
32Mpbs
C)
36Mpbs
D)
72Mpbs

Correct Answer :   72Mpbs


Explanation : For binary transmission, the maximum theoretical data rate or channel capacity C for a given bandwidth B is C = 2B = 2(36) =72Mpbs.

A)
ANIK
B)
WESTAR
C)
MOLNIYA
D)
EARLY BIRD (Intelsat-I)

Correct Answer :   EARLY BIRD (Intelsat-I)

A)
wobbling
B)
three-axis stabilization
C)
drift from stationary position
D)
three-dimensional stabilization

Correct Answer :   wobbling

A)
30
B)
100
C)
270
D)
0

Correct Answer :   30

A)
Time Division Multiple Access (TDMA)
B)
Code Division Multiple Access (CDMA)
C)
Frequency Division Multiple Access (FDMA)
D)
All of the above

Correct Answer :   All of the above

8 .
Assuming earth to be a sphere of radius 6400 km and height of a geosynchronous satellite above Earth as 36000 km, the velocity of a geosynchronous satellite is __________ km/hr.
A)
11100
B)
15000
C)
28000
D)
36000

Correct Answer :   11100

A)
500
B)
1000
C)
5000
D)
100000

Correct Answer :   100000

A)
100
B)
50
C)
20
D)
10

Correct Answer :   20

A)
Automatic Relay Request
B)
Automatic Repeat Request
C)
Accelerated Recovery Request
D)
Automatic Radiation Quenching

Correct Answer :   Automatic Repeat Request

A)
Relay satellites
B)
Repeater satellites
C)
Communication satellites
D)
Geosynchronous satellites

Correct Answer :   Communication satellites


Explanation : Communication satellites are not originators of information to be transmitted. If a transmitting station cannot communicate directly with one or more receiving stations because of line-of-sight restrictions, a satellite can be used. The transmitting station sends the information to the satellite, which in turn re-transmits it to the receiving stations.

A)
Relay
B)
Duplexer
C)
Repeater
D)
Transponder

Correct Answer :   Transponder


Explanation : The transmitter-receiver combination in the satellite is known as a transponder. The basic functions of a transponder are amplification and frequency translation. The reason for frequency translation is that the transponder cannot transmit and receive on the same frequency.

A)
LNA
B)
TWT
C)
Satellite dish
D)
Helical antenna

Correct Answer :   Satellite dish

A)
Path loss
B)
RFI
C)
Radiation loss
D)
Atmospheric loss

Correct Answer :   Path loss

A)
Cost
B)
Privacy
C)
Access
D)
Coverage

Correct Answer :   Privacy

A)
More gain
B)
Redundancy
C)
Better reception
D)
More number of operating channel

Correct Answer :   More number of operating channel


Explanation : To be economically feasible, a satellite must be capable of handling several channels. As a result, most satellites contain multiple transponders, each operating at a different frequency. Each transponder represents an individual communication channel.

A)
More bandwidth
B)
Economically viable
C)
More spectrum space
D)
Are not diffracted by the ionosphere

Correct Answer :   Are not diffracted by the ionosphere


Explanation : VHF, UHF, and microwave signals penetrate the ionosphere with little or no attenuation and are not refracted to earth. Lower frequencies undergo total internal refraction and get reflected back to earth.

A)
Increases
B)
Decreases
C)
Remains the same
D)
None of the above

Correct Answer :   Increases

A)
Spot beam
B)
Zone beam
C)
Global beam
D)
Hemispheric beam

Correct Answer :   Global beam

A)
Digital Analog Master Antenna
B)
Demand-Assigned Multiple Access
C)
Dynamically-Assigned Multiple Access
D)
Decibel Attenuated Microwave Access

Correct Answer :   Demand-Assigned Multiple Access

A)
17.34°
B)
51.4°
C)
60°
D)
120°

Correct Answer :   17.34°

A)
273
B)
243
C)
170
D)
123

Correct Answer :   123

A)
Rohini
B)
Apple
C)
Bhaskara
D)
Aryabhatta

Correct Answer :   Apple

26 .
The INTELSAT-IV satellite launched in 1974 had two earth coverage antenna and two narrower-angle antennas subtending 4.5°. The signal from narrow-angle antenna was stronger than that from earth- coverage antenna by a factor of
A)
17.34/4.5
B)
17.34 x 4.5
C)
(17.34/4.5)²
D)
(17.34/4.5)⁴

Correct Answer :   (17.34/4.5)²

A)
has a circular orbit
B)
rotates in the equatorial plane
C)
has the same period a that of the Earth
D)
has all of the above

Correct Answer :   has all of the above

A)
retransmits the received signal
B)
changes the frequency of the received signal
C)
does all of the above-mentioned functions
D)
receives a signal from Earth station and amplifies

Correct Answer :   does all of the above-mentioned functions

A)
Only two side bands are needed
B)
Upper side band and part of carrier are needed
C)
Both side bands and full-amplitude carrier are needed
D)
One side band and full-ampiitude carrier are needed

Correct Answer :   Both side bands and full-amplitude carrier are needed

A)
noise power to bandwidth
B)
antenna gain to frequency
C)
transmission losses to noise
D)
information-carrying capacity to S/N ratio

Correct Answer :   noise power to bandwidth

A)
More bandwidth
B)
Overcrowding
C)
Lesser attenuation
D)
Less power requirements

Correct Answer :   Overcrowding


Explanation : Most new communication satellites will operate in the Ku band. This upward shift in frequency is happening because the C band is overcrowded. Many communication satellites are in orbit now, most of them operating in the C band. However, there is some difficulty with interference because of the heavy usage. The only way this interference will be minimized is to shift all future satellite communication to higher frequencies.

A)
More gain
B)
High speed
C)
Error detection
D)
Reduce traffic load

Correct Answer :   Reduce traffic load


Explanation : at times there is more traffic than there are transponders to handle it. For that reason, numerous techniques have been developed to effectively increase the bandwidth and signal-carrying capacity of the satellite. Two of these techniques are known as frequency reuse and spatial isolation.

A)
Stub
B)
Balun
C)
Microstrip tapers
D)
Quarter-wavelength transformer

Correct Answer :   Quarter-wavelength transformer

A)
Uplink
B)
Terrestrial
C)
Downlink
D)
Earthbound

Correct Answer :   Downlink

A)
1979
B)
1981
C)
1983
D)
1985

Correct Answer :   1979

A)
L-band
B)
C-band
C)
X-band
D)
Ku-band

Correct Answer :   C-band

A)
Gain
B)
Beamwidth
C)
Maneuverability
D)
Circular polarization

Correct Answer :   Circular polarization

A)
its footprint must be increased
B)
the number of its feed horns must be increased
C)
the frequency of its transmission must be increased
D)
its effective isotropic radiated power (EIRP) must be increased

Correct Answer :   the frequency of its transmission must be increased

A)
2
B)
10
C)
88
D)
277

Correct Answer :   88

A)
UK
B)
USA
C)
USSR
D)
None of the above

Correct Answer :   USA

A)
a form of commutator
B)
a device for digitizing speech
C)
a circuit used for suppressing microwave mterference
D)
an electronic circuit which carries out modulation and demodulation of a carrier frequency

Correct Answer :   an electronic circuit which carries out modulation and demodulation of a carrier frequency

A)
Only one side band and part of carrier is suppressed
B)
Carrier is completely suppressed
C)
Both side hands are suppressed
D)
One side band and full carrier is suppressed

Correct Answer :   Only one side band and part of carrier is suppressed

A)
watts
B)
picowatts
C)
kilowatts
D)
milliwatts

Correct Answer :   picowatts

A)
launch takes place eastward
B)
the satellite achieves circular orbit quickly
C)
spent rocket motor and other launcher debris falls into the sea
D)
expenditure of propulsion fuel is reduced during plane changing

Correct Answer :   spent rocket motor and other launcher debris falls into the sea

46 .
The owner of a communication satellite is usually required to keep the spacecraft on station at its assigned place in the geosynchronous orbit with an accuracy of __________ degree.
A)
0.1
B)
0.5
C)
1.0
D)
2.0

Correct Answer :   0.1

A)
INSAT-IA
B)
INSAT-IB
C)
INSAT-IC
D)
INSAT-ID

Correct Answer :   INSAT-IB

A)
time multiplexing
B)
space multiplexing
C)
Both (A) and (B)
D)
frequency multiplexing

Correct Answer :   frequency multiplexing

A)
one frequency is used as a back up for the other
B)
the system operates at a mean frequency of 5 GHz
C)
4 GHz is the down-link and 6 GHz is the up-link frequency
D)
4 GHz is the up-link and 6 GHz is the down-link frequency

Correct Answer :   4 GHz is the down-link and 6 GHz is the up-link frequency

A)
Spatial isolation
B)
Modulation
C)
Multiplexing
D)
Frequency reuse

Correct Answer :   Spatial isolation


Explanation : By using narrow beam or spot beam antennas, the area on the earth covered by the satellite can be divided up into smaller segments. Earth stations in each segment may actually use the same frequency, but because of the very narrow beam widths of the antennas, there is no interference between adjacent segments.

A)
Modulation
B)
Multiplexing
C)
Spatial isolation
D)
Frequency reuse

Correct Answer :   Frequency reuse


Explanation : In the frequency reuse technique two systems use the same frequency, although operating on exactly the same frequencies, they are isolated from each other by the use of special antenna techniques.

For example, a vertically polarized antenna will not respond to a horizontally polarized signal and vice versa. Or a left-hand circularly polarized (LHCP) antenna will not respond to a right-hand circularly polarized (RHCP) signal and vice versa.

A)
True
B)
False
C)
Can Not Say
D)
None of the above

Correct Answer :   True


Explanation : Spatial-division multiple access uses spatial isolation technique. Earth stations in each segment may actually use the same frequency, but because of the very narrow beam widths of the antennas, there is no interference between adjacent segments.

This technique is referred to a spatial-division multiple access (SDMA) in that access to the satellite depends on location and not frequency.

A)
True
B)
False
C)
Can Not Say
D)
None of the above

Correct Answer :   True


Explanation : The original signal being transmitted from the earth station to the satellite is called the uplink, and the re-transmitted signal from the satellite to the receiving stations is called the downlink.

Usually, the downlink frequency is lower than the uplink frequency. A typical uplink frequency is 6 GHz, and a common downlink frequency is 4 GHz.

A)
Solar jet
B)
Liquid fuel
C)
Jet propulsion
D)
Ion propulsion system

Correct Answer :   Ion propulsion system

A)
Zone
B)
Footprint
C)
Bandwidth
D)
Beamwidth

Correct Answer :   Footprint

A)
Lithium
B)
Leclanche
C)
Hydrogen
D)
Magnesium

Correct Answer :   Hydrogen

A)
500 MHz
B)
500 GHz
C)
1000 MHz
D)
1000 GHz

Correct Answer :   500 MHz

A)
105.5° East
B)
115.5° East
C)
151.5° East
D)
170.5° East

Correct Answer :   105.5° East

A)
IMPATT
B)
Zener diode
C)
Shockley diode
D)
Tunnel diode

Correct Answer :   Tunnel diode

A)
TWT
B)
Transponders
C)
Trancievers
D)
Transducers

Correct Answer :   Transponders

A)
3.85
B)
14.85
C)
78
D)
220

Correct Answer :   220

A)
It gives preferential treatment to the weaker parts of the signal
B)
Weaker signals, traverse more quantum steps than they would do otherwise and so quantizing error is reduced.
C)
For weaker signals it gives a poor ratio of signal strength to quantizing error
D)
It compresses the higher-amplitude parts of a signal before modulation and expands them back to normal again after demodulation.

Correct Answer :   For weaker signals it gives a poor ratio of signal strength to quantizing error

A)
Though it is more efficient than TASI, it is much slower
B)
It is a digital form of TASI
C)
A speaker has to wait (it at all) for only a few milliseconds for reallocation of channel
D)
It has increased the capacity of satellite channels by a factor of 2.2 or more with out degrading speech quality

Correct Answer :   Though it is more efficient than TASI, it is much slower

A)
Bangalore in South India
B)
Cape Canaveral in Florida
C)
Kourou in French Guyana
D)
Canarvon in Western Australia

Correct Answer :   Kourou in French Guyana

A)
470
B)
540
C)
270
D)
100

Correct Answer :   540

A)
For fixed antenna, it is inversely proportional to f2
B)
Loss in down-link is negligible as compared to that in uplink
C)
For a given satellite operating at a given frequency, it is inversely proportional to
D)
For fixed frequency, it is inversely proportional to the product of the antenna aperture areas

Correct Answer :   Loss in down-link is negligible as compared to that in uplink

A)
permits the use of smaller antenna
B)
does not suffer from rain attenuation
C)
does not suffer from atmospheric at tenuation
D)
offers a much wider available bandwidth

Correct Answer :   offers a much wider available bandwidth

A)
C/N
B)
G/T
C)
S/N
D)
EIRP

Correct Answer :   C/N

A)
1989-90
B)
1991-92
C)
1992-93
D)
1993-94

Correct Answer :   1989-90

A)
EHF
B)
UHF
C)
SHF
D)
VHF

Correct Answer :   SHF

A)
sun
B)
earth
C)
moon
D)
All of the above

Correct Answer :   All of the above

A)
2
B)
25 and 60
C)
30 and 82.5
D)
40 and 92.5

Correct Answer :   40 and 92.5

A)
loss of power
B)
battery power provision
C)
eclipse period
D)
mass of station-keeping fuel

Correct Answer :   battery power provision

A)
sun-synchronous polar
B)
polar
C)
equatorial
D)
geostationary

Correct Answer :   sun-synchronous polar

A)
EIRP
B)
antenna size
C)
coverage a sea
D)
antenna gain

Correct Answer :   coverage a sea

A)
it is resistant to the effects of noise
B)
demodulation is very easy
C)
phase can be varied from + 180° to 180°
D)
it gives highest data rates that can be transmitted over a given channel

Correct Answer :   it is resistant to the effects of noise

A)
Silicon based panel
B)
Galium Arsenide solar panel array
C)
Germanium based panels
D)
Galium Phosphate solar panel array

Correct Answer :   Galium Arsenide solar panel array

A)
Leclanche
B)
Lithium
C)
Hydrogen
D)
Magnesium

Correct Answer :   Lithium

A)
5°
B)
17°
C)
21°
D)
35°

Correct Answer :   17°

A)
2225 MHz
B)
2555 MHz
C)
3500 MHz
D)
4500 MHz

Correct Answer :   2225 MHz

A)
Series
B)
Radial
C)
Shunt
D)
Matrix

Correct Answer :   Shunt

A)
does not wait for acknowledgement after sending a block
B)
sends another block if positive acknowledge is received through ACK character
C)
resends the previous block if negative acknowledgement is received through a NAK character
D)
waits for positive or negative acknowled-gement from the receiving terminal after sending a block

Correct Answer :   does not wait for acknowledgement after sending a block

A)
100
B)
500
C)
1000
D)
2000

Correct Answer :   1000

A)
remains stationary above the Earth
B)
travels around the Earth in 24 hours
C)
hangs motionless in space about 36000 km about Earth
D)
appears stationary to everybody on Earth

Correct Answer :   appears stationary to everybody on Earth

A)
a transmitting station and a receiving station
B)
a transmitting station and many receiving station
C)
many transmitting station and many receiving station
D)
None of the above

Correct Answer :   many transmitting station and many receiving station

A)
27.5 to 30
B)
5 to 10
C)
10 to 15
D)
30 to 50

Correct Answer :   27.5 to 30

A)
key leverage
B)
spread-spectrum modulation
C)
once-only key
D)
frequency hopping

Correct Answer :   spread-spectrum modulation

A)
WESTAT
B)
INSAT-IC
C)
INSAT-ID
D)
ARABSAT

Correct Answer :   ARABSAT

A)
collection of meteoric dust
B)
increase in resistivity of silicon
C)
their bombardment by electrons
D)
gradual leakage of charge carriers from the semiconductor material

Correct Answer :   their bombardment by electrons

A)
maximise antenna gain
B)
minimise free-space losses
C)
avoid interference from terrestrial microwave links
D)
avoid interference between its powerful transmitted signal and weak in coming signal

Correct Answer :   avoid interference between its powerful transmitted signal and weak in coming signal

A)
echo suppressor
B)
a vocoder
C)
a multiplexer
D)
digital techniques

Correct Answer :   echo suppressor

A)
intelligence gathering capacity
B)
domestic communications
C)
meteorological capability
D)
Both (B) and (C)

Correct Answer :   Both (B) and (C)

A)
INSAT-2
B)
Olympus-I
C)
INSAT-ID
D)
Intelsat-V

Correct Answer :   Olympus-I

A)
Divider/combiner
B)
Radial combiner
C)
Radial divider
D)
Radial multiplexer

Correct Answer :   Radial divider

A)
4 - 8 GHz
B)
8 - 12 GHz
C)
12 - 18 GHz
D)
26 - 40 GHz

Correct Answer :   12 - 18 GHz

A)
Perigee
B)
Zenith
C)
Apogee
D)
Prograde

Correct Answer :   Perigee

A)
TDMA
B)
CDMA
C)
ANIK-D
D)
FDMA

Correct Answer :   FDMA

A)
Intel Satellite
B)
International Satellite
C)
International Telephone Satellite
D)
International Telecommunications Satellite

Correct Answer :   International Telecommunications Satellite

A)
Satellite-to-earth link
B)
Satellite-to-satellite link
C)
Earth-to-satellite link
D)
None of the above

Correct Answer :   Satellite-to-satellite link

101 .
A colour television signal having bandwidth of 4.6 MHz is digitised using 10 bits sample. The digital bit rate used for its transmission with PCM would be __________ kilobits/second.
A)
230
B)
920
C)
23000
D)
92000

Correct Answer :   92000

A)
Leh
B)
Madras
C)
Hassan
D)
New Delhi

Correct Answer :   Hassan

A)
5
B)
300
C)
10000
D)
35900

Correct Answer :   35900

A)
5 minutes on 10 consecutive days
B)
10 minutes on 5 consecutive days
C)
30 minutes for 5 consecutive days
D)
one hour for 5 consecutive days

Correct Answer :   10 minutes on 5 consecutive days

A)
large bandwidth and severe noise
B)
high modulation index
C)
small bandwidth and negligible noise
D)
maximum bandwidth and minimum noise

Correct Answer :   large bandwidth and severe noise

A)
gives better beam-shaping
B)
results in lesser signal attenuation
C)
gives a narrow beam shining into space
D)
is easier to polarize a high frequency beam

Correct Answer :   gives a narrow beam shining into space

A)
Oblateness of the Earth
B)
Pressure of solar radiations
C)
Weight of the satellite
D)
Gravitational changes due to Sun and Moon

Correct Answer :   Weight of the satellite

A)
34 and 106
B)
52 and 88
C)
34 and 142
D)
106 and 142

Correct Answer :   52 and 88

A)
1
B)
3
C)
5
D)
10

Correct Answer :   3

A)
36000
B)
33070
C)
22800
D)
11200

Correct Answer :   11200

A)
heat up and melt
B)
produce sonic booms
C)
do not provide 24 hour/ day contact to the users on Earth
D)
None of the above

Correct Answer :   heat up and melt

A)
500
B)
303
C)
254
D)
100

Correct Answer :   254

A)
strengthen the beam to overcome the cosmic noise
B)
direct the spot beam to a particular region of space on Earth
C)
make corrections in change of polarisation of the beam
D)
select a particular channel in transmission and reception

Correct Answer :   direct the spot beam to a particular region of space on Earth

A)
ARABSAT
B)
INSAT-2
C)
INSAT-ID
D)
INSTELSAT-V

Correct Answer :   ARABSAT

A)
135
B)
270
C)
540
D)
1080

Correct Answer :   270

A)
50
B)
40
C)
20
D)
10

Correct Answer :   10

A)
modem
B)
codec
C)
compandor
D)
transponder

Correct Answer :   codec

A)
its EIRP
B)
satellite antenna gain
C)
noise associated with the satellite
D)
All of the above

Correct Answer :   All of the above

A)
Sun and satellite
B)
Sun and Earth station
C)
Satellite and Earth station
D)
Sun, satellite and Earth station

Correct Answer :   Sun, satellite and Earth station

A)
global communication
B)
24-hour orbit
C)
stationary satellite
D)
zero-gravity environs

Correct Answer :   global communication

A)
1 hours
B)
12 hours
C)
24 hours
D)
48 hours

Correct Answer :   24 hours

A)
0.8
B)
3
C)
18
D)
30

Correct Answer :   0.8

A)
Zone beam
B)
Spot beam
C)
Global beam
D)
Hemispheric beam

Correct Answer :   Spot beam

A)
Courier
B)
Explorer
C)
Early Bird
D)
Telstar

Correct Answer :   Telstar

A)
Prograde satellite
B)
Retrograde satellite
C)
Nonsynchronous satellite
D)
Geosynchronous satellite

Correct Answer :   Nonsynchronous satellite

A)
24
B)
30
C)
48
D)
50

Correct Answer :   30

A)
Sputnik I
B)
Echo I
C)
Telstar I
D)
Early Bird

Correct Answer :   Sputnik I

A)
6
B)
12
C)
14
D)
80

Correct Answer :   14

A)
Japan Satellite System (JSAT)
B)
Singapore Satellite Commision
C)
Asia Satellite Telecommunications Company (ASTC)
D)
China Great Wall Industry Corporation

Correct Answer :   China Great Wall Industry Corporation

A)
22,426.4 miles
B)
23,426.4 miles
C)
26,426.4 miles
D)
27,426.4 miles

Correct Answer :   22,426.4 miles