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IMPACT Project IMPACT Project

IMPACT Project - PowerPoint Presentation

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Uploaded On 2016-06-27

IMPACT Project - PPT Presentation

Drag coefficients of Low Earth Orbit satellites computed with the Direct Simulation Monte Carlo method Andrew Walker ISR1 LAUR 1224986 Outline Motivation Direct Simulation Monte Carlo DSMC method ID: 379927

closed form surface accommodation form closed accommodation surface coefficient solutions cll energy dac analysis gas sensitivity satellite dsmc sensitive

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