Classical Mechanics and Newtonian Dynamics
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A rocket moves in deep space (ignore gravity). It ejects fuel at constant speed \(u\) relative to the rocket. At \(t=0\), the rocket has mass \(m_0\) and speed \(v_0\) in an inertial frame. Fuel is expelled at a constant rate \(\dot m=-k\) (so \(m(t)=m_0-kt\)). What is the rocket speed \(v(t)\) for \(0\le t< m_0/k\)?
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