JPL Technical Report Server

Ulysses Orbit Determination at High Declinations

Show simple item record

dc.contributor.author McElrath, Timothy P. en_US
dc.contributor.author Lewis, George D. en_US
dc.date.accessioned 2004-10-02T17:56:55Z
dc.date.available 2004-10-02T17:56:55Z
dc.date.issued 1995-05 en_US
dc.identifier.citation NASA/GSFC Flight Dynamics Conference en_US
dc.identifier.citation Greenbelt, MD en_US
dc.identifier.clearanceno 95-0590 en_US
dc.identifier.uri http://hdl.handle.net/2014/29970
dc.description.abstract The trajectory of the Ulysses spacecraft caused its geocentric declination to en_US
dc.format.extent 520671 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.title Ulysses Orbit Determination at High Declinations en_US


Files in this item

This item appears in the following Collection(s)

Show simple item record

Search


Browse

My Account