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Low Earth orbit constellation design using the Earth-Moon L1 point

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dc.contributor.author Chow, Naomi
dc.contributor.author Gralla, Erica
dc.contributor.author Kasdin, N. J.
dc.date.accessioned 2005-11-09T21:25:36Z
dc.date.available 2005-11-09T21:25:36Z
dc.date.issued 2004-02
dc.identifier.citation Space Flight Mechanics Meeting, Hawaii, February 8-12, 2004 en
dc.identifier.clearanceno 04-0407
dc.identifier.uri http://hdl.handle.net/2014/37921
dc.description.abstract This paper presents a proof of concept an feasibility assessment of such a system, demonstrating 38% cost savings for a baseline mission. en
dc.description.sponsorship NASA en
dc.format.extent 1269371 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US en
dc.publisher Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2004. en
dc.subject microsatellites en
dc.subject microsatellite constellations en
dc.subject L1 trajectories en
dc.title Low Earth orbit constellation design using the Earth-Moon L1 point en
dc.type Preprint en


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