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Results tagged with rocket-equation
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user 32826
Equation stating that the change in velocity (delta-v) of a single stage rocket is equal to the exhaust velocity times the natural log of the ratio of final to initial mass, named after Russian scientist Konstantin Tsiolkovsky.
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Can I exclude coriolis effects if I express a rocket launch in an inertial reference frame f...
I am wondering if I can exclude coriolis effects and centrifugal forces if I calculate my position relative to an inertial reference frame with as origin the launch site at the moment of lift off. Dir …
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