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Particular impulse subsequently has deep impacts to the achievable delta-v and affiliated orbits achievable, and (because of the rocket equation) mass fraction required to realize a presented delta-v. Optimizing the tradeoffs concerning mass fraction and unique impulse is one of the basic engineering challenges in rocketry. A rocket should https://simonxnanz.articlesblogger.com/55411851/the-basic-principles-of-isp

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