blake_ch20.pdf

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    Chapter 20: Satellite Communications  

    MULTIPLE CHOICE 

    1. The height of the geosynchronous orbit above the equator is about:

    a. 3,578 km c. 357,800 km

    b. 35,780 km d. depends on satellite velocity

    ANS: B

     

    2. The high and low points of a satellite's orbit are called, respectively,:

    a. apogee and perigee c. uplink and downlink

    b. perigee and apogee d. downlink and uplink

    ANS: A

     

    3. The area on the earth that is "covered" by a satellite is called its:

    a. earth station c. footprintb. downlink d. plate

    ANS: C

     

    4. The velocity required to stay in orbit:

    a. is constant

    b. is zero (freefall)

    c. is lower close to the earth than far from the earth

    d. is higher close to the earth than far from the earth

    ANS: D 

    5. An antenna is aimed by adjusting the two "look angles" called:a. azimuth and elevation c. declination and elevation

    b. azimuth and declination d. apogee and perigee

    ANS: A

     

    6. The power per transponder of a typical Ku-band satellite is in the range:

    a. 5 to 25 watts c. 500 to 2500 watts

    b. 50 to 250 watts d. depends on its orbit

    ANS: B

     

    7. The power level for an earth station to transmit to a satellite is on the order of:

    a. 101 watts c. 103 wattsb. 102 watts d. 104 watts

    ANS: C

     

    8. The "payload" on a communications satellite consists of:

    a. transponders c. solar cells

    b. batteries d. all of the above

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    ANS: A 

    9. "Station-keeping" refers to:

    a. antenna maintenance c. orbital adjustments

    b. power-level adjustments d. none of the above

    ANS: C 

    10. DBS stands for:

    a. decibels of signal c. direct-broadcast system

    b. down-beam signal d. direct-broadcast satellite

    ANS: D

     

    11. LNA stands for:

    a. low-noise amplifier c. low-noise amplitude

    b. low north angle d. low-noise array

    ANS: A

     12. A reduction in TWT power for linearity is called:

    a. backdown c. power-down

    b. backoff d. EIRP drop

    ANS: B

     

    13. TVRO stands for:

    a. television receive only c. television remote origin

    b. television repeater only d. none of the above

    ANS: A

     

    14. TDMA stands for:a. transponder-directed multiple antennas c. time-division multiple access

    b. television distribution master antenna d. transmit delay minimum aperture

    ANS: C 

    15. VSAT stands for:

    a. video satellite c. very small antenna terminal

    b. video signal antenna terminal d. very small aperture terminal

    ANS: D

     

    16. On the uplink from a terminal, a VSAT system uses:

    a. high power to a small antenna c. low power to a large antenna

    b. low power to a small antenna d. LEO satellites

    ANS: B

     

    17. A typical VSAT system is configured as a:

    a. star c. ring

    b. mesh d. repeater

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    ANS: A 

    18. LEO stands for:

    a. long elliptic orbit c. lateral earth orbit

    b. low-earth orbit d. longitudinal earth orbit

    ANS: B 

    19. For real-time communication, LEO systems require:

    a. a constellation of satellites c. very high power

    b. tracking dish antennas d. all of the above

    ANS: A

     

    20. The frequency bands used by Ku-band satellites are:

    a. 4 GHz and 6 GHz c. 20 GHz and 30 GHz

    b. 12 GHz and 14 GHz d. none of the above

    ANS: B

     COMPLETION

     1. A satellite in geosynchronous orbit takes ____________________ hours to complete one orbit. 

    ANS: 24

    2. The ____________________ is the signal path from the earth station to the satellite. 

    ANS: uplink

    3. The ____________________ is the signal path from the satellite to the earth station. 

    ANS: downlink

    4. A satellite in a ____________________ orbit appears to stay directly above one spot on the equator. 

    ANS: geostationary

    5. Non-geostationary satellites are sometimes called ____________________ satellites. 

    ANS: orbital

    6. A geosynchronous orbit is about ____________________ km above the earth. 

    ANS: 35,780

    7. A ____________________ is an outline of the area on the earth's surface that a satellite broadcasts to. 

    ANS: footprint

    8. All satellite orbits are ____________________ in shape. 

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    ANS: elliptical

    9. The ____________________ is the distance of a satellite's closest approach to the earth. 

    ANS: perigee

    10. The ____________________ is a satellite's farthest distance from the earth. 

    ANS: apogee

    11. An antenna's ____________________ is its angular direction between east and west. 

    ANS: azimuth

    12. An antenna's ____________________ is its vertical angle with respect to the earth's surface.  

    ANS: elevation

    13. An antenna's ____________________ is the angle by which it is offset from the earth's axis. 

    ANS: declination

    14. Satellites using the ____________________ band operate on 12 GHz. 

    ANS: Ku

    15. The time for a signal to make a round trip via satellite is about ____________________ milliseconds. 

    ANS: 500

    16. A ____________________ is a type of repeater used on communications satellites. 

    ANS: transponder

    17. Both the gain and the beamwidth of a dish antenna depend on its ____________________. 

    ANS: diameter

    18. VSAT systems commonly use a ____________________ network configuration. 

    ANS: star

    19. To date, LEO satellite systems have been a financial ____________________. 

    ANS: failure

    20. C-band antennas are ____________________ than Ku-band antennas.  

    ANS: larger

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     SHORT ANSWER

     

    1. A receiving antenna with a gain of 44.4 dBi looks at a sky with a noise temperature of 15 K. The loss

    between the output of the antenna and the input of the LNA is 0.4 dB, and the LNA has a noise

    temperature of 40 K. Calculate the G/T. 

    ANS:

    25 dB

     

    2. A receiver has a noise figure of 1.7 dB. Find its equivalent noise temperature. 

    ANS:

    139 K. 

    3. A receiving antenna with a G/T of 25 dB is used to receive signals from a satellite 38,000 km away. Thesatellite has a 100-watt transmitter and an antenna with a gain of 30 dBi. The signal has a bandwidth of 1

    MHz at a frequency of 12 GHz. Calculate the C/N at the receiver. 

    ANS:

    38 dB