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Ispaceplus - An Overview

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"In genuine rocket nozzles, the exhaust velocity is not really uniform about your complete exit cross portion and these velocity profiles are challenging to evaluate precisely. A uniform axial velocity, ve, is assumed for all calculations which employ one-dimensional difficulty descriptions. This efficient exhaust velocity represents an average or mass https://damienqhugt.blog-eye.com/33141103/not-known-facts-about-isp

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