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SIRTF trajectory design and optimization

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dc.contributor.author Garcia, M. D. en_US
dc.date.accessioned 2004-09-22T22:27:36Z
dc.date.available 2004-09-22T22:27:36Z
dc.date.issued 2001-02-11 en_US
dc.identifier.citation AAS/AIAA Space Flight Mechanics Meeting en_US
dc.identifier.citation Santa Barbara, CA, USA en_US
dc.identifier.clearanceno 01-0348 en_US
dc.identifier.uri http://hdl.handle.net/2014/12311
dc.description.abstract This paper examines why direct ascent is not an option for the summer launch, presents the new launch/injection strategy, and discusses the solar orbit optimization criteria used to define viable solar orbits. en_US
dc.format.extent 914474 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other solar orbit direct ascent parking orbit injection targets operational pointing zone en_US
dc.title SIRTF trajectory design and optimization en_US


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