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Ultralight linerless composite tanks for the In-Space applications

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dc.contributor.author Mallick, Kaushik
dc.contributor.author Tupper, Michael L.
dc.contributor.author Grimes-Ledesma, Lorie
dc.contributor.author Lewis, Joseph C.
dc.contributor.author Welsh, Jeffry
dc.date.accessioned 2006-04-12T17:53:05Z
dc.date.available 2006-04-12T17:53:05Z
dc.date.issued 2004-09-28
dc.identifier.citation AIAA Space 2004, San Diego, California, September 28-30, 2004. en
dc.identifier.clearanceno 04-0123
dc.identifier.uri http://hdl.handle.net/2014/39027
dc.description.abstract A program has been proposed to NASA to develop a technology that will provide helium containment a the high strain levels required to create low mass tanks for in-space propulsion applications. The specific goal of the program is to develop linerless composite tanks that will successfully contain small molecule gases, such as, He, at 10,000 psia for a target mission life or 15 years. en
dc.description.sponsorship NASA/JPL en
dc.format.extent 183344 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 lightweight propellant tanks en
dc.subject composite tanks en
dc.title Ultralight linerless composite tanks for the In-Space applications en
dc.type Preprint en


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