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3 years ago

10

If the rocket burns its fuel in a time of 50.0 s and the relative speed of the exhaust gas is vex = 2100 m/s, what must the mass

ratio m0/m be for a final speed v of 8.00 km/s (about equal to the orbital speed of an earth satellite)?

1 answer:

Flauer [41]3 years ago

4 0

Answer:

f = 45.13

Explanation:

Check the attached file for the solution

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