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The isp Diaries

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[38] When the actual exhaust velocity is reduced for air-respiration engines, the successful exhaust velocity is rather high for jet engines. It is because the efficient exhaust velocity calculation assumes which the carried propellant is supplying each of the reaction mass and each of the thrust. As a result successful https://troyguitg.targetblogs.com/33515637/considerations-to-know-about-ispaceplus

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