Principles of communications satellites
Explains the reasons, limitations and trade-offs inherent to communications satellites. The first half deals with link power budgets as well as communications hardware and examples of complete link budgets. Spacecraft technology and a description of the objectives and basic operating methods of each of the major supporting subsystems are covered in the last half. Contains end-of-chapter exercises and solutions.
An Instructor's Manual presenting detailed solutions to all the problems in the book is available from the Wiley editorial department.
53 pages matching error in this book
Results 1-3 of 53
Introduction To Link Budgets
Orbits For Communications Satellites
16 other sections not shown
angular momentum antenna diameter antenna gain attenuation attitude control bandwidth battery beam Boltzmann's constant calculated carrier-to-noise ratio command communications satellites components configuration factor constant curve dBHz dBi/K dBW/K decibels density distance downlink earth sensor earth station earth station antenna EIRP electron elevation angle emissivity equation error example failure rate figure of merit free space path frequency function G/Ts gain G geostationary orbit geostationary satellite heat hydrazine illumination level increase input INTELSAT launch link budget longitude mass maximum modulation momentum wheel noise power operating oscillation parameters path loss pitch polarization power amplifier radiation radius range receive antenna reflector reliability rotation satel shown in Figure signal solar array solar cells space path loss spacecraft subsatellite point subsystem surface Table telemetry thermal thrusters tion torque transmitter power transponder units uplink usually velocity voltage wavelength wheel