DC Field | Value | Language |
---|---|---|
dc.contributor.author | Cho, IH | - |
dc.contributor.author | Baek, Seung-Wook | - |
dc.contributor.author | Chang, ST | - |
dc.date.accessioned | 2013-03-15T13:14:29Z | - |
dc.date.available | 2013-03-15T13:14:29Z | - |
dc.date.created | 2012-02-06 | - |
dc.date.issued | 1996-07 | - |
dc.identifier.citation | The 32nd AIAA/ASME/SAE/ ASEE Joint Propulsion Conference, v., no., pp. - | - |
dc.identifier.uri | http://hdl.handle.net/10203/119761 | - |
dc.language | ENG | - |
dc.title | A Numerical Simulation of Axisymmetric Solid Rocket Motor Ignition Transient with Radiation Effect | - |
dc.type | Conference | - |
dc.type.rims | CONF | - |
dc.citation.publicationname | The 32nd AIAA/ASME/SAE/ ASEE Joint Propulsion Conference | - |
dc.identifier.conferencecountry | United States | - |
dc.identifier.conferencecountry | United States | - |
dc.contributor.localauthor | Baek, Seung-Wook | - |
dc.contributor.nonIdAuthor | Cho, IH | - |
dc.contributor.nonIdAuthor | Chang, ST | - |
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