Explore topic-wise InterviewSolutions in .

This section includes InterviewSolutions, each offering curated multiple-choice questions to sharpen your knowledge and support exam preparation. Choose a topic below to get started.

1.

What provides the sufficient drive to the final power amplifier?(a) Intermediate-power amplifier(b) Operational amplifier(c) Power driver circuit(d) Up converterI got this question at a job interview.My enquiry is from Satellite Applications topic in division Satellite Communication of Avionics

Answer»

Correct CHOICE is (a) Intermediate-POWER amplifier

Explanation: The power amplifier USUALLY BEGINS with an initial stage called the intermediate-power amplifier (IPA). This PROVIDES sufficient drive to the final high-power amplifier (HPA).

2.

Which frequency band is used for connecting the satellite system with the public switched telephone network?(a) L band(b) Ku band(c) C band(d) Ka bandI had been asked this question during an interview.This interesting question is from Satellite Applications in division Satellite Communication of Avionics

Answer»

The CORRECT answer is (d) Ka band

To EXPLAIN: The satellites communicate with ground stations called gateways that connect the system to the public switched TELEPHONE network. The satellites also communicate among themselves. Both gateway and intersatellite COMMUNICATION TAKES place over Ka band frequencies.

3.

What technique does DSP use to double the number of channels by using helical antennas?(a) Spatial isolation(b) Frequency reuse(c) Multiplexing(d) ModulationI had been asked this question during an interview.This interesting question is from Satellite Applications topic in division Satellite Communication of Avionics

Answer»

Correct OPTION is (b) Frequency reuse

The explanation is: The digital SIGNAL is transmitted from the satellite to the receivers using circular polarization. The DBS satellites have right-hand and left-hand circularly polarized (RHCP and LHCP) helical antennas. By TRANSMITTING both polarities of signal, frequency reuse can be incorporated to double the channel CAPACITY.

4.

What is the number of satellites present in the Iridium system?(a) 72(b) 51(c) 66(d) 32I had been asked this question in final exam.My query is from Satellite Applications topic in chapter Satellite Communication of Avionics

Answer»

Correct answer is (c) 66

Explanation: The satellite systems use low-earth-orbit satellites to perform the relay services to the main TELEPHONE system or to make a connection directly between any TWO cellular telephones USING the system. One of the oldest and most widely used is the Iridium system. It uses a CONSTELLATION of 66 satellites in six polar orbits with 11 satellites per orbit 420 mi above the earth.

5.

Which frequency band does the direct broadcast satellite system use?(a) C band(b) X band(c) Ku band(d) MF bandI have been asked this question by my school teacher while I was bunking the class.My question comes from Satellite Applications topic in division Satellite Communication of Avionics

Answer»

Correct choice is (C) Ku band

The best EXPLANATION: The DBS satellite uses the Ku band with a frequency range of 11 to 14 GHz. UPLINK SIGNALS are usually in the 14- to 14.5-GHz range, and the downlink usually covers the range of 10.95 to 12.75 GHz.

6.

What type of satellite TV service uses compressed data transmission to beam signals directly to every home?(a) Direct broadcast satellite(b) Mobile satellite service(c) Broadcasting satellite service(d) Fixed satellite serviceI have been asked this question during an interview.My query is from Satellite Applications in section Satellite Communication of Avionics

Answer»

The correct CHOICE is (a) Direct broadcast satellite

The best explanation: The direct broadcast satellite (DBS) system is an all-digital system. Data compression techniques are used to reduce the data rate in ORDER to produce high-quality picture and sound. They uses special broad COVERAGE SATELLITES with high power to transmit cable-TV-like SERVICES direct to homes equipped with the special DBS receivers.

7.

Which of the following is not a reason for redistributing TV signals through satellites rather than skywaves or spacewaves?(a) High frequency signal(b) Long distance communication(c) Economically feasible(d) Power requirementsI got this question in homework.Enquiry is from Satellite Applications in section Satellite Communication of Avionics

Answer»

The CORRECT option is (d) POWER requirements

Easiest explanation: TV signals are being TRANSMITTED through satellites for redistribution. Because of the very high-frequency signals involved in TV transmission, other long-distance transmission methods are not technically or economically FEASIBLE.

8.

What is the primary use of communication satellites?(a) Telephone service(b) Surveillance(c) Research(d) GPSThis question was addressed to me in examination.I'd like to ask this question from Satellite Applications topic in division Satellite Communication of Avionics

Answer»

Right CHOICE is (a) Telephone service

Explanation: The PRIMARY use of communication satellites is in long-distance telephone service. Satellites greatly SIMPLIFY long-distance CALLS not only within countries but ALSO worldwide.

9.

When individual up converters are used to modulate a channel, what is used to combine them into final signal?(a) Microwave combiner(b) Multiplexer(c) Mixer(d) AmplifierThe question was asked during an interview for a job.I'd like to ask this question from Ground Stations in portion Satellite Communication of Avionics

Answer»

Correct choice is (a) MICROWAVE COMBINER

To EXPLAIN: Individual up CONVERTERS are used on each modulated CHANNEL. At the output of the up converters, all the signals are combined in a microwave combiner, which produces a single output signal that is fed to the final amplifiers.

10.

In digital systems, analog signals are first digitized with PCM converters before modulation.(a) True(b) FalseI have been asked this question in examination.My question is based upon Ground Stations in division Satellite Communication of Avionics

Answer»

Right ANSWER is (a) True

Easy EXPLANATION: In digital systems, ANALOG signals are first digitized with PCM converters. The resulting serial digital OUTPUT is then used to modulate a QPSK modulator.

11.

In RF tuning, _________ provides the final up conversion to the microwave frequency?(a) Fixed-frequency local oscillator(b) RF frequency synthesizer(c) Quartz oscillator(d) Magnetic oscillatorThe question was posed to me in class test.My query is from Ground Stations topic in section Satellite Communication of Avionics

Answer»

Correct answer is (b) RF frequency synthesizer

For explanation I would SAY: In RF TUNING, a mixer FED by a fixed-frequency local oscillator performs an initial up conversion to 700 MHz. Then a sophisticated RF frequency synthesizer applied to a second mixer provides up conversion to the final MICROWAVE frequency.

12.

Which of the following amplifiers is used in the transmitter substation?(a) RF amplifiers(b) Buffer amplifiers(c) Klystron amplifier(d) Operational amplifiersThe question was posed to me in semester exam.The doubt is from Ground Stations topic in portion Satellite Communication of Avionics

Answer»

Right answer is (c) Klystron amplifier

To elaborate: The signals to be sent to the satellite MIGHT be TV programs, multiple TELEPHONE calls, or DIGITAL data from a COMPUTER. These signals are used to modulate the carrier, which is then amplified by a large traveling-wave TUBE or klystron amplifier.

13.

Which part of the transmitter subsystem modulates the baseband signal?(a) Antenna(b) Up converter(c) Power amplifiers(d) MixerThis question was addressed to me during a job interview.My doubt stems from Ground Stations topic in section Satellite Communication of Avionics

Answer»

The correct option is (b) Up converter

To ELABORATE: The transmit subsystem consists of two BASIC parts, the up CONVERTERS and the POWER amplifiers. The up converters translate the BASEBAND signals modulated on to carriers up to the final uplink microwave frequencies.

14.

If the earth station downlink signal received is at fs = 4.08 GHz, what first stage local-oscillator frequency fLO is needed to achieve IF of 770 MHz?(a) 3310 MHz(b) 4080 MHz(c) 1203 MHz(d) 3250 MHzThis question was addressed to me at a job interview.The query is from Ground Stations topic in division Satellite Communication of Avionics

Answer» RIGHT ANSWER is (a) 3310 MHz

To EXPLAIN: FIF = fs – fLO

fLO = fs – fIF = 4080 – 770 = 3310 MHz.
15.

The satellite in the earth station must be steerable even for a geosynchronous satellite.(a) True(b) FalseThe question was posed to me in an interview for job.This intriguing question originated from Ground Stations topic in division Satellite Communication of Avionics

Answer»

Right option is (a) True

To elaborate: It must be possible to adjust its AZIMUTH and elevation so that the antenna can be properly ALIGNED with the satellite. Earth stations supporting geosynchronous satellites can generally be fixed in position, HOWEVER, azimuth and elevation adjustments are necessary to initially PINPOINT the satellite and to permit minor adjustments over the satellite’s life.

16.

In Rf tuning, what is the first local oscillator?(a) Quartz oscillator(b) Frequency synthesizer(c) Magnetic oscillator(d) Electric oscillatorsThe question was asked in homework.I need to ask this question from Ground Stations topic in chapter Satellite Communication of Avionics

Answer»

Right choice is (b) FREQUENCY SYNTHESIZER

Easiest explanation: In RF tuning, the first local oscillator is made adjustable. Generally, a frequency synthesizer is USED in this application. The frequency synthesizer GENERATES a HIGHLY stable signal at selected frequency increments.

17.

What is the use of the band pass filter in the receiver section?(a) Protects the receiver(b) Increases antenna gain(c) Reduces noise(d) To reduce it to an intermediate frequencyI got this question during a job interview.This intriguing question comes from Ground Stations in portion Satellite Communication of Avionics

Answer»
18.

Telemetry, command, and control (TC&C) subsystem allow a ground station to monitor and control conditions in the satellite.(a) True(b) FalseThis question was posed to me in an interview for internship.I need to ask this question from Satellite Subsystems in division Satellite Communication of Avionics

Answer»

Correct option is (a) True

To EXPLAIN I would say: The telemetry system is used to report the status of the onboard subsystems to the ground station. The telemetry system typically consists of various ELECTRONIC sensors WHOSE data are SELECTED by a multiplexer and then converted to a digital signal, which then modulates an internal TRANSMITTER. This transmitter sends the telemetry information back to the earth station, where it is recorded and monitored.

19.

Which of the following is not true?(a) Battery is only used as a back up(b) When in orbit, solar power is always available(c) Battery is used for initial satellite orientation and stabilization(d) The batteries are charged using solar powerThe question was posed to me in class test.My question is from Satellite Subsystems in division Satellite Communication of Avionics

Answer»

Right option is (b) When in orbit, solar POWER is always available

Best explanation: When a SATELLITE goes into an ECLIPSE or when the solar panels are not properly POSITIONED, there is a temporary cut in solar power supply. In situations like this the batteries take over temporarily and keep the satellite operating. The batteries are not large enough to power the satellite for a long time; they are used as a backup system for ECLIPSES, initial satellite orientation and stabilization, or emergency conditions.

20.

Why is it not possible to provide transmit function by wideband amplifier and mixer circuits?(a) Heavy attenuation(b) High power output over wideband is not possible(c) Economically not profitable(d) Weight of the system increases five foldThis question was addressed to me in a national level competition.The origin of the question is Satellite Subsystems topic in division Satellite Communication of Avionics

Answer»

Right option is (b) High power OUTPUT over wideband is not POSSIBLE

Explanation: it is generally not possible to generate very high output power over such wide bandwidth. The FACT is that no components and circuits can do this well. The high-power amplifiers in most transponders are traveling-wave tubes that inherently have limited bandwidth. They operate well over a small RANGE but cannot DEAL with the entire 500-MHz bandwidth allocated to a satellite.

21.

What is the number of transponders if the satellite uses 12 channels of frequency and frequency reuse is implemented?(a) 12(b) 6(c) 24(d) 3I had been asked this question in an online quiz.My question comes from Satellite Subsystems topic in section Satellite Communication of Avionics

Answer»

Correct OPTION is (c) 24

The explanation is: Since in frequency REUSE each channel can be used TWICE the numbers of transponders are also DOUBLED. 12 x 2 = 24 transponders, two for each frequency.

22.

In a regenerative transponder, the signal is demodulated and modulated again before transmission.(a) True(b) FalseI have been asked this question during an interview for a job.My question is taken from Satellite Subsystems in division Satellite Communication of Avionics

Answer»

The correct choice is (a) True

The BEST explanation: A regenerative REPEATER demodulates the uplink SIGNAL after the frequency is translated to some lower intermediate frequency. The RECOVERED baseband signal is then used to modulate the downlink signal.

23.

Which of the following transponders convert the uplink signal to downlink signal using two mixers(a) Single conversion transponders(b) Dual conversion transponders(c) Regenerative transponders(d) Dual mixer transponderI got this question in quiz.The query is from Satellite Subsystems in portion Satellite Communication of Avionics

Answer»

Correct choice is (b) Dual conversion transponders

The BEST I can explain: A dual-conversion TRANSPONDER makes the FREQUENCY translation in two STEPS with two MIXERS. No demodulation occurs.

24.

Which of the following components receives, translates the signal frequency and re-transmits the signal in a satellite?(a) Repeater(b) Relay(c) Transponder(d) TransducerThe question was posed to me in my homework.The doubt is from Satellite Subsystems in section Satellite Communication of Avionics

Answer»

Correct choice is (c) Transponder

The EXPLANATION is: The uplink SIGNALS from EARTH are amplified, translated in frequency, and re-transmitted on the downlink to ONE or more earth STATIONS. The component that performs this function is known as a transponder.

25.

Which of the following are common baseband signals transmitted from the earth ground station?(a) Navigational data, computer data, video(b) Computer data, navigational data, voice(c) Voice, video, computer data(d) Computer dataI have been asked this question by my school teacher while I was bunking the class.The query is from Satellite Subsystems topic in portion Satellite Communication of Avionics

Answer»

Right answer is (c) Voice, video, computer DATA

Best EXPLANATION: An earth station takes the signals to be transmitted, known as baseband signals, and MODULATES a microwave CARRIER. The three most common baseband signals are voice, video, and computer data.

26.

Why is there a huge spectrum space between the transmitted and received signal in satellite communication?(a) Reduce interference(b) Maximum efficiency(c) Less attenuation(d) To reduce space occupied by filtersI have been asked this question in an interview for internship.My question is taken from Satellite Subsystems topic in chapter Satellite Communication of Avionics

Answer»

Correct option is (a) Reduce interference

For explanation I would say: Because of the CLOSE proximity of the transmitter and the receiver in the satellite, the high transmitter output power for the downlink is picked up by that satellite receiver. Naturally, the uplink SIGNAL is totally obliterated. Furthermore, the transmitter output FED back into the receiver input causes oscillation. To avoid this PROBLEM, the receiver and transmitter in the satellite TRANSPONDER are designed to operate at separate frequencies. In this way, they will not interfere with each other.

27.

Which of the following is not a part of the propulsion subsystem of a satellite?(a) Gyroscope(b) Jet thruster(c) AKM(d) Fuel control systemThe question was asked in semester exam.The above asked question is from Satellite Subsystems in section Satellite Communication of Avionics

Answer» RIGHT ANSWER is (a) Gyroscope

Easy EXPLANATION: The propulsion subsystem consists of the AKM(Apogee kick motor), jet thruster and the fuel control system. GYROSCOPES and other attitude SYSTEMS fall under the attitude control subsystem.
28.

Spatial-division multiple access (SDMA) depends on satellite location and not frequency.(a) True(b) FalseThis question was addressed to me by my school principal while I was bunking the class.Enquiry is from Satellite Communication Systems topic in chapter Satellite Communication of Avionics

Answer»

Correct answer is (a) True

Easiest 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.

29.

Which technique uses two different antennas to reduce traffic on the same frequency?(a) Spatial isolation(b) Frequency reuse(c) Multiplexing(d) ModulationThe question was posed to me at a job interview.My question is based upon Satellite Communication Systems topic in chapter Satellite Communication of Avionics

Answer»

Correct ANSWER is (b) Frequency reuse

Easy 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.

30.

Which of the following is not a satellite subsystem?(a) Ground station(b) Power system(c) Telemetry tracking(d) Communication subsystemI had been asked this question in my homework.Origin of the question is Satellite Subsystems in portion Satellite Communication of Avionics

Answer»

Right option is (a) Ground station

Explanation: The communication subsystem is the most IMPORTANT part of the satellite. It requires VARIES additional systems like the POWER system, propulsion system, telemetry system for its proper FUNCTIONING. The ground system HOWEVER is not one of the satellite subsystem and is independent of the satellite. It is just a transponder to monitor and command the satellite.

31.

Which technique uses spot beam antennas to divide the area covered by the satellite into smaller segments?(a) Spatial isolation(b) Frequency reuse(c) Multiplexing(d) ModulationI had been asked this question in an interview for internship.I want to ask this question from Satellite Communication Systems topic in portion Satellite Communication of Avionics

Answer»

Right answer is (a) Spatial isolation

The explanation is: 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.

32.

What is the maximum theoretical data rate if a transponder is used for binary transmission and has a bandwidth of 36MHz?(a) 32Mpbs(b) 72Mpbs(c) 36Mpbs(d) 12MpbsThe question was posed to me during an interview for a job.Asked question is from Satellite Communication Systems in division Satellite Communication of Avionics

Answer»

Correct CHOICE is (b) 72Mpbs

For explanation: For binary transmission, the maximum theoretical data RATE or CHANNEL capacity C for a given BANDWIDTH B isC = 2B = 2(36) =72Mpbs.

33.

Why are techniques like frequency reuse and spatial isolation carried out?(a) Reduce traffic load(b) More gain(c) High speed(d) Error detectionI got this question by my school principal while I was bunking the class.This is a very interesting question from Satellite Communication Systems topic in division Satellite Communication of Avionics

Answer» RIGHT answer is (a) Reduce traffic load

The 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.
34.

Which of the following bands cannot be used for satellite communication?(a) MF(b) Ku(c) X(d) CI have been asked this question in an international level competition.I would like to ask this question from Satellite Communication Systems in chapter Satellite Communication of Avionics

Answer»

The CORRECT answer is (a) MF

To explain: 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.

35.

Why are VHF, UHF, and microwave signals used in satellite communication?(a) More bandwidth(b) More spectrum space(c) Are not diffracted by the ionosphere(d) Economically viableI got this question during an online exam.Origin of the question is Satellite Communication Systems topic in section Satellite Communication of Avionics

Answer»

Right answer is (c) Are not diffracted by the IONOSPHERE

The EXPLANATION is: 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.

36.

What is the reason for shifting from c band to ku band in satellite communication?(a) Lesser attenuation(b) Less power requirements(c) More bandwidth(d) OvercrowdingThe question was posed to me by my school principal while I was bunking the class.The above asked question is from Satellite Communication Systems in portion Satellite Communication of Avionics

Answer»

The CORRECT option is (d) Overcrowding

To elaborate: 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.

37.

The satellite that is used as a relay to extend communication distance is called as __________(a) Relay satellites(b) Communication satellites(c) Repeater satellites(d) Geosynchronous satellitesThe question was posed to me in exam.The question is from Satellite Communication Systems in division Satellite Communication of Avionics

Answer»

The CORRECT ANSWER is (B) Communication satellites

The explanation is: 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.

38.

What is the reason for carrying multiple transponders in a satellite?(a) More number of operating channel(b) Better reception(c) More gain(d) RedundancyI had been asked this question during an interview.The above asked question is from Satellite Communication Systems topic in portion Satellite Communication of Avionics

Answer»

Right choice is (a) More number of OPERATING channel

Easy 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.

39.

The transmitter-receiver combination in the satellite is known as a _______(a) Relay(b) Repeater(c) Transponder(d) DuplexerI have been asked this question during an online interview.This intriguing question originated from Satellite Communication Systems in chapter Satellite Communication of Avionics

Answer»

Right answer is (c) 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.

40.

What is the point on the surface of the earth that is directly below the satellite called?(a) Satellite point(b) Subsatellite point(c) Supersatellite point(d) Overhead pointThe question was asked in a job interview.The doubt is from Satellite Orbits topic in portion Satellite Communication of Avionics

Answer»

Correct ANSWER is (B) Subsatellite point

To elaborate: The satellite location is specified by a point on the surface of the EARTH DIRECTLY below the satellite. This point is known as the subsatellite point (SSP). The subsatellite point is then located by using conventional latitude and LONGITUDE designations.

41.

The downlink frequency is lower than the uplink frequency.(a) True(b) FalseThe question was posed to me by my school teacher while I was bunking the class.My doubt is from Satellite Communication Systems in chapter Satellite Communication of Avionics

Answer»

Correct answer is (a) True

The explanation is: 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.

42.

The angle between the line from the earth station’s antenna to the satellite and the line between the earth station’s antenna and the earth’s horizon is called as ___________(a) Angle of inclination(b) Angle of elevation(c) Apogee angle(d) LOS angleI got this question in an interview for job.My question is from Satellite Orbits topic in section Satellite Communication of Avionics

Answer»

The correct CHOICE is (b) Angle of elevation

Best explanation: The angle of elevation of a satellite is the angle that APPEARS between the line from the earth station’s antenna to the satellite and the line between the earth station’s antenna and the earth’s horizon. If the angle of elevation is too small, the signals between the earth station and the satellite have to pass through MUCH more of the earth’s atmosphere. Because of the very low powers USED and the high absorption of the earth’s atmosphere.

43.

To use a satellite for communication relay or repeater purposes what type of orbit will be the best?(a) Circular orbit(b) Elliptical orbit(c) Geosynchronous orbit(d) Triangular orbitThis question was posed to me at a job interview.The above asked question is from Satellite Orbits topic in chapter Satellite Communication of Avionics

Answer»

The correct choice is (c) GEOSYNCHRONOUS orbit

Best explanation: The best SOLUTION is to launch a synchronous or GEOSTATIONARY satellite. In a geosynchronous earth orbit. Since the satellite remains apparently fixed, no special earth station tracking antennas are REQUIRED. The antenna is simply pointed at the satellite and remains in a fixed position. With this ARRANGEMENT, continuous communication is possible.

44.

What percentage of the earth can communication satellites see?(a) 20(b) 50(c) 70(d) 40The question was asked by my college professor while I was bunking the class.I need to ask this question from Satellite Orbits in section Satellite Communication of Avionics

Answer»

Right option is (d) 40

To elaborate: Most COMMUNICATION satellites in USE today are of the geosynchronous variety. Approximately 40 percent of the earth’s SURFACE can be “seen” or accessed from such a satellite. Users INSIDE that area can use the satellite for communication.

45.

What is the angle of inclination for a satellite following an equatorial orbit?(a) 0°(b) 180°(c) 45°(d) 90°This question was addressed to me by my college director while I was bunking the class.My question comes from Satellite Orbits topic in division Satellite Communication of Avionics

Answer»

The correct option is (a) 0°

For EXPLANATION: Another DEFINITION of inclination is the angle between the equatorial plane and the satellite ORBITAL plane as the satellite enters the northern HEMISPHERE. When the angle of inclination is 0°, the satellite is directly above the equator. Orbits with 0° inclination are generally called equatorial orbits.

46.

The period of time that elapses between the successive passes of the satellite over a given meridian of earth longitude is called as _____________(a) synodic period(b) Lapsed time(c) Time period(d) Sidereal periodI have been asked this question during a job interview.The origin of the question is Satellite Orbits topic in portion Satellite Communication of Avionics

Answer»

Correct answer is (a) synodic PERIOD

Explanation: ANOTHER method of expressing the time for one orbit is the revolution or synodic period. One revolution (1 r) is the period of time that elapses between the successive passes of the SATELLITE over a given meridian of earth LONGITUDE. Naturally, the synodic and sidereal periods differ from each other because of the earth’s ROTATION.

47.

The time period taken by the satellite to complete one orbit is called ________(a) Lapsed time(b) Time period(c) Sidereal period(d) Unit frequencyThis question was addressed to me in an interview for internship.My enquiry is from Satellite Orbits topic in division Satellite Communication of Avionics

Answer»

Right option is (c) Sidereal PERIOD

The best I can explain: The period is the time it TAKES for a satellite to complete one ORBIT. It is also called the sidereal period. A sidereal orbit uses some external fixed or apparently motionless object such as the sun or star for REFERENCE in determining a sidereal period.

48.

Satellites closer to the earth travel at lower speeds than satellites that are far away from earth.(a) True(b) FalseThis question was posed to me in a national level competition.Asked question is from Satellite Orbits topic in chapter Satellite Communication of Avionics

Answer»

Correct answer is (B) False

Easiest explanation: Satellites that are near earth have to move at HIGHER SPEEDS to sustain their orbit since the gravitational pull is much higher. Since the EFFECT of gravity is less at higher altitudes, satellites that far away REQUIRE less speeds.

49.

When is the speed of the satellite maximum in an elliptical orbit?(a) Retrograde(b) Posigrade(c) Perigee(d) ApogeeI have been asked this question in quiz.This intriguing question originated from Satellite Orbits in section Satellite Communication of Avionics

Answer»

Right CHOICE is (c) Perigee

The explanation is: In an elliptical orbit, the speed changes depending upon the height of the satellite above the earth. Naturally, the speed of the satellite is greater when it is CLOSE to the earth than when it is far AWAY. The CLOSEST POINT is called the perigee.

50.

The direction of orbit in the same direction of earth rotation is called ______(a) Retrograde(b) Posigrade(c) Perigee(d) ApogeeI had been asked this question by my school principal while I was bunking the class.The doubt is from Satellite Orbits topic in section Satellite Communication of Avionics

Answer»

Correct OPTION is (b) Posigrade

For explanation: The direction of SATELLITE rotation may be either in the same direction as the EARTH’s rotation or against the direction of earth’s rotation. In the former case, the orbit is said to be posigrade, and in the latter case, retrograde. Most ORBITS are posigrade.