Show simple item record

dc.contributor.authorLalloobhai, Amit Desaien_US
dc.date.accessioned2013-07-22T20:15:06Z
dc.date.available2013-07-22T20:15:06Z
dc.date.issued2013-07-22
dc.date.submittedJanuary 2013en_US
dc.identifier.otherDISS-12197en_US
dc.identifier.urihttp://hdl.handle.net/10106/11871
dc.description.abstractThe scope of this research is the design and development of a self-stabilizing re-entry vehicle that closely resembles naturally occurring seeds in nature. It was hypothesized that a femto-satellite with a shape of a samara could self stabilize and passively generate lift, as well as transmit a signal during its descent through the atmosphere. The research included a conceptual design phase and a preliminary design phase that entailed analytic simulations, and an experimental demonstration. The goal was to investigate the feasibility of developing the above-mentioned femto-vehicle that could increase the range capability of its descent to maximize data capture.en_US
dc.description.sponsorshipHarris, Benen_US
dc.language.isoenen_US
dc.publisherAerospace Engineeringen_US
dc.titleThe Samara Spacecraft: Design And Development Of A Self-stabilizing, Auto-rotating, Distributed Sensing Systemen_US
dc.typeM.S.en_US
dc.contributor.committeeChairHarris, Benen_US
dc.degree.departmentAerospace Engineeringen_US
dc.degree.disciplineAerospace Engineeringen_US
dc.degree.grantorUniversity of Texas at Arlingtonen_US
dc.degree.levelmastersen_US
dc.degree.nameM.S.en_US


Files in this item

Thumbnail


This item appears in the following Collection(s)

Show simple item record