A rocket fully loaded with fuel has total mass
including mass
of fuel. The rocket is fired vertically upwards at
. During its journey, the fuel is allowed to burn at a constant rate
such that the relative backward velocity of the exhaust gases is
.
(a) If
is the mass of the rocket plus fuel and
its velocity at time
, show that, if air resistance is neglected, the equation of motion is
.
(b) Show that, the speed of the rocket at time
is given by
.
(c) The height
which is reached by the rocket at the instant when the fuel is all burnt depends on the rate of burning
. Determine the rate of burning
such that the height reached will be maximal. (Hint: For the stationary value to be maximal, first show that

at
)
Roughwork.
(a) Jot
. Take
. By Newton’s 2nd law,

(b)

and the result follows.
(c) From
![Rendered by QuickLaTeX.com \begin{aligned} v(t) & = -gt-u\ln \bigg( 1-\frac{b}{M}t\bigg) \\ H(t) & =\int_0^t v(t')\,\mathrm{d}t' \\ & = \int_0^t \bigg[ -gt'-u\ln \bigg( 1-\frac{b}{M}t'\bigg) \bigg]\,\mathrm{d}t' \\ & = -\frac{g}{2}t'^2\bigg|_0^t +\frac{uM}{b}\int_{t'=0}^{t'=t} \ln T\,\mathrm{d}T \\ \dots\enspace & \textrm{as }\int \ln x\,\mathrm{d}x=x\ln x-x+C\enspace \dots \\ \end{aligned}](https://physicspupil.com/wp-content/ql-cache/quicklatex.com-e45aa5ccd805e16aca30c5f9fea6435c_l3.svg)
This problem is not to be attempted.