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COROT mission

COROT mission. Orbit parameters Two orbit models are used at system level inertial polar circular orbit right ascension of the ascending node :  = 12.5° ( ± 180 ) altitude 826 km ( a = 7204 km ) altitude 900 km ( a = 7278 km ) preferred for phase properties (orbit cycle of 7 / 14 days)

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Experiences of Grid Enabled MPI Implementation named MPICH-GX with Atmospheric Applications

Experiences of Grid Enabled MPI Implementation named MPICH-GX with Atmospheric Applications. Oh-kyoung Kwon, KISTI Salvador Castañeda, CICESE. PRAGMA 11. Contents. Motivation KISTI’s Proposal MPICH-GX Experiments Next things to do. Atmospheric Applications. MM5

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228 views • 10 slides

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