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Isp - An Overview

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"In genuine rocket nozzles, the exhaust velocity is not really uniform around the whole exit cross area and such velocity profiles are difficult to evaluate accurately. A uniform axial velocity, ve, is assumed for all calculations which utilize a single-dimensional challenge descriptions. This effective exhaust velocity represents an average or https://pragmaticplay-slots45666.spintheblog.com/33402977/the-best-side-of-ispace-casino

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