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dc.contributor.advisorStecher, George J.
dc.contributor.authorBartlein, Andrew R.
dc.contributor.authorBrewer, Nicholas R.
dc.contributor.authorVasel, Justin A.
dc.date.accessioned2011-11-30T14:41:05Z
dc.date.available2011-11-30T14:41:05Z
dc.date.issued2011-05
dc.identifier.urihttp://digital.library.wisc.edu/1793/55360
dc.descriptionColor poster with text and graphs.en
dc.description.abstractChanging the orbit of a spacecraft requires large changes in energy and angular momentum. If a spacecraft approaches a target planet with too much angular momentum, it will be routed around the planet and not captured into orbit. To be captured, the spacecraft must shed excess energy. A method called "aerobraking" can be used to slow the spacecraft down by letting it pass through the upper atmosphere of a planet to burn off excess energy. This study examines the parameters needed to break a spacecraft around Neptune using the process of aerobraking.en
dc.description.sponsorshipUniversity of Wisconsin--Eau Claire Office of Research and Sponsored Programsen
dc.language.isoen_USen
dc.relation.ispartofseriesUSGZE AS589en
dc.subjectNeptune (Planet)--Orbiten
dc.subjectAerothermodynamicsen
dc.subjectSpace vehiclesen
dc.subjectPostersen
dc.titleAchieving a Closed Orbit Around Neptune Through Aerobrakingen
dc.typePresentationen


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  • Student Research Day
    Posters of collaborative student/faculty research presented at Student Research Day

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