Page 256 - Satellite Communications, Fourth Edition
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236  Chapter Seven

                              7.11.  Briefly describe the equipment sections making up a transponder
                              channel.

                              7.12.  Draw to scale the uplink and downlink channeling schemes for a
                              500-MHz-bandwidth C-band satellite, accommodating the full complement
                              of 36-MHz-bandwidth transponders. Assume the use of 4-MHz guardbands.

                              7.13.  Explain what is meant by frequency reuse, and describe briefly two
                              methods by which this can be achieved.

                              7.14.  Explain what is meant by  redundant receiver  in connection with
                              communication satellites.

                              7.15.  Describe the function of the input demultiplexer used aboard a
                              communications satellite.

                              7.16.  Describe briefly the most common type of high-power amplifying device
                              used aboard a communications satellite.

                              7.17. What is the chief advantage of the TWTA used aboard satellites compared
                              to other types of high-power amplifying devices? What are the main
                              disadvantages of the TWTA?

                              7.18.  Define and explain the term 1-dB  compression point. What is the
                              significance of this point in relation to the operating point of a TWTA?

                              7.19.  Explain why operation near the saturation point of a TWTA is to be
                              avoided when multiple carriers are being amplified simultaneously.

                              7.20. State the type of satellite antenna normally used to produce a widebeam
                              radiation pattern, providing global coverage. How are spot beams produced?

                              7.21.  Describe briefly how beam shaping of a satellite antenna radiation
                              pattern may be achieved.

                              7.22.  With reference to Figure 7.28, explain what is meant by a four-for-two
                              redundancy switching arrangement.


                              References

                              CCIR. 1984. Fixed Services Handbook, final draft. Geneva.
                              Chetty, P. R. K. 1991. Satellite Technology and Its Applications. McGraw-Hill, New York.
                              Hyndman, J. E. 1991. Hughes HS601 Communications Satellite Bus System Design
                                 Trades. Hughes Aircraft Company, El Segundo, CA.
                              Johnston, E. C., and J. D. Thompson. 1982. “INTELSAT VI Communications Payload.”
                                 IEE Colloquium on the Global INTELSAT VI Satellite System, Digest No. 1982/76.
                                 pp. 4/1–4/4.
                              Lilly, C. J. 1990. “INTELSAT’s New Generation.” IEE Review, Vol. 36, No. 3, March.
                                 pp. 111–113.
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