burnt out speed and thurst of rocket
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Explanation:
the rocket thrust is x10^ N. which gives vburnout = m/s. Fowles and Cassiday give as example data for a satellite launch a low orbit velocity of about 8 km/s, an initial velocity of about 0.5 km/s from the rotation of the earth near the equator, and an exhaust velocity of 2.5 km/s.
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