M5 June 2018 Q5
5. At time \(t = 0\) a rocket is launched. The rocket has initial mass \(M\), of which mass \(\lambda M\), \(0 \lt \lambda \lt 1\), is fuel. The rocket is launched vertically upwards, from rest, from the surface of the Earth. The rocket burns fuel and the burnt fuel is ejected vertically downwards with constant speed \(U\) relative to the rocket. At time \(t\), the rocket has mass \(m\) and velocity \(v\). Ignoring air resistance and any variation in \(g\),
The rocket accelerates vertically upwards with constant acceleration \(g\).
| Scheme | Marks |
|---|---|
| \((m + \delta m)(v + \delta v) + (-\delta m)(v - U) - mv = -mg\,\delta t\) | M1 A2 |
| \(mv + v\,\delta m + m\,\delta v + U\,\delta m - v\,\delta m - mv = -mg\,\delta t\) | |
| \(m\dfrac{\mathrm{d}v}{\mathrm{d}t} + U\dfrac{\mathrm{d}m}{\mathrm{d}t} = -mg\) GIVEN ANSWER | A1 |
| (4) |
Notes
First M1 for use of Impulse-Momentum principle, dimensionally correct, with correct no. of terms, with usual rules.
First and second A1 for a correct equation
Third A1 for the correct given answer correctly obtained.
| Scheme | Marks |
|---|---|
| \(mg + U\dfrac{\mathrm{d}m}{\mathrm{d}t} = -mg\) | |
| \(U\dfrac{\mathrm{d}m}{\mathrm{d}t} = -2mg\) | M1 |
| \(\displaystyle\int_M^m \dfrac{\mathrm{d}m}{m} = \dfrac{-2g}{U}\int_0^t \mathrm{d}t\) | M1 |
| \(\left[\ln m\right]_M^m = \dfrac{-2gt}{U}\) | A1 |
| \(m = M\mathrm{e}^{\frac{-2gt}{U}}\) GIVEN ANSWER | A1 |
| (4) |
Notes
First M1 for putting \(\dfrac{\mathrm{d}v}{\mathrm{d}t} = g\) into the DE and collecting terms
Second M1 for separating the variables and attempting to integrate both sides
First A1 for a correct integral on both sides with correct limits oe
Second A1 for the GIVEN ANSWER correctly obtained.
| Scheme | Marks |
|---|---|
| \((1 - \lambda)M = M\mathrm{e}^{\frac{-2gT}{U}}\) | M1 |
| \(T = \dfrac{U}{2g}\ln\left(\dfrac{1}{1 - \lambda}\right)\) | A1 |
| \(v = gT = \dfrac{U}{2}\ln\left(\dfrac{1}{1 - \lambda}\right)\) | M1 A1 |
| \(\text{KE} = \dfrac{1}{2}(1 - \lambda)M\left[\dfrac{U}{2}\ln\left(\dfrac{1}{1 - \lambda}\right)\right]^2 = \dfrac{1}{8}MU^2(1 - \lambda)\left[\ln\left(\dfrac{1}{1 - \lambda}\right)\right]^2\) | M1 A1 |
| (6) | |
| (14 marks) |
Notes
First M1 for putting \(m = (1 - \lambda)M\) and solving for \(T\)
First A1 for a correct expression for \(T\)
Second M1 for using \(v = u + at\) oe with \(u = 0\), \(a = g\) and \(t\) = their \(T\) to find \(v\)
Second A1 for a correct \(v\)
Third M1 for use of KE formula (M0 if they use \(M\) for mass)
Third A1 for a correct expression in any form.