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A-B-Cs of sun-synchronous orbit mission designThe paper will develop the background and information necessary to explain what a sun-synchronous orbit is how it works. Handy back of the envelope equations will be provided to enable the mission analyst and system engineer to do quick and simple calculations for the orbit parameters selection and to compute mission parameters important to satellite design without having to resort to sophisticated computer programs.
Document ID
20210001902
Acquisition Source
Jet Propulsion Laboratory
Document Type
Preprint (Draft being sent to journal)
External Source(s)
Authors
Boain, Ronald J.
Date Acquired
February 1, 2004
Publication Date
February 1, 2004
Publication Information
Publisher: Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2004.
Distribution Limits
Public
Copyright
Other
Technical Review

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