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Abstract

A communications satellite has two conflicting requirements. It must have sufficient altitude to give geometrical coverage of the Earth’s surface, but not be so high that the inverse square law overpowers the extra coverage due to extra height. Thus the orbits in this paper are independent of the launching rocket used, although published data for the British Blue Streak-Black Knight rocket combination has been used to indicate the variation of satellite weight for various altitudes and orbits.

Keywords

Circular Orbit Elliptic Orbit Communication Purpose Precession Rate Inertial Space 
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.

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References

  1. [1]
    R. P. Haviland,Astronautica Acta, 4: 1 (1958).Google Scholar
  2. [2]
    S. R. Dauncey,Hawker Siddeley Aviation Limited., APG/4007/0801 (April, 1960).Google Scholar
  3. [3]
    B. Stewart,Hawker Siddeley Aviation Limited., APG/4007/0102 (March, 1960).Google Scholar
  4. [4]
    D. G. King-Hele,Proceedings of the Royal Society, (A) 247, p. 49 (1958).Google Scholar

Copyright information

© Springer-Verlag Wien 1961

Authors and Affiliations

  • W. F. Hilton
    • 1
  • S. R. Dauncey
    • 1
  1. 1.Hawker Siddeley Aviation LimitedKingston-upon-Thames, SurreyEngland

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