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Satellite Configuration Design

  • Gasser F. Abdelal
  • Nader Abuelfoutouh
  • Ahmed H Gad
Chapter

Abstract

This chapter discusses the process of integration of the subsystem components and development of the satellite configuration to achieve a final layout for a satellite; the process will be applied on a test case and it is called “Small Sat”. The Small Sat structural configuration is designed to accommodate all of the mission components. All mechanical requirements are derived from the satellite’s configuration. The process used to create the satellite configuration of Small Sat is described. It begins with mission definition, launch vehicle selection, and subsystem identification. This is followed by a description of the satellite composition, and the major design constraints that guide the configuration design. Then a configuration development process is presented to create the preliminary configuration. Finally, the issued layout drawings and the calculated mass properties for the developed satellite are presented.

Keywords

Solar Panel Launch Vehicle Solar Array Satellite Configuration Reaction Wheel 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

References

  1. 1.
    Sarafin TP, Larson WJ (eds) (1995) Spacecraft structures and mechanisms—from concept to launch. Microcosm Press and Kluwer Academic Publishers, Torrance, CAGoogle Scholar
  2. 2.
    Dnepr SLS User’s Guide, Issue 2, Nov. 2001. http://www.kosmotras.ru

Copyright information

© Springer-Verlag London 2013

Authors and Affiliations

  • Gasser F. Abdelal
    • 1
  • Nader Abuelfoutouh
    • 2
  • Ahmed H Gad
    • 3
  1. 1.Aerospace and Manufacturing DepartmentQueen’s University BelfastBelfastUK
  2. 2.Faculty of EngineeringCairo UniversityCairoEgypt
  3. 3.National Authority for Remote Sensing and Space SciencesEgyptian Space ProgramCairoEgypt

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