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A rocket that is 85% fuel by mass launches from the surface of Mars. Its exhaust velocity has
a constant value of u = 2.9 × 103 m s−1.
Determine the maximum launch duration if the rocket is to achieve a delta-v ▲v =
3.3 km s
−1
-2
The acceleration due to gravity on Mars may be assumed to be a constant 3.71 m s−2.
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Transcribed Image Text:A rocket that is 85% fuel by mass launches from the surface of Mars. Its exhaust velocity has a constant value of u = 2.9 × 103 m s−1. Determine the maximum launch duration if the rocket is to achieve a delta-v ▲v = 3.3 km s −1 -2 The acceleration due to gravity on Mars may be assumed to be a constant 3.71 m s−2.
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