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A spaceship's orbital maneuver requires a speed increase of 1.40 10 3 m/s. If its engine has an exhaust speed of 2.00 10 3 m/s,
A spaceship's orbital maneuver requires a speed increase of 1.40 103 m/s. If its engine has an exhaust speed of 2.00 103 m/s, determine the required ratio
Mi |
Mf |
of its initial mass to its final mass. (The difference
Mi Mf
equals the mass of the ejected fuel.)
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