Edexcel M3 2024 January — Question 1 6 marks

Exam BoardEdexcel
ModuleM3 (Mechanics 3)
Year2024
SessionJanuary
Marks6
PaperDownload PDF ↗
Mark schemeDownload PDF ↗
TopicAdvanced work-energy problems
TypeInverse-square gravitational force
DifficultyStandard +0.3 This is a standard M3 gravitational mechanics question requiring integration of F=ma with variable force. Part (a) is a straightforward 'show that' using separation of variables (v dv/dx = acceleration), and part (b) substitutes given values to find C then evaluates at x=R. The setup is clearly guided with all necessary information provided, making it slightly easier than average for A-level.
Spec3.02f Non-uniform acceleration: using differentiation and integration6.02c Work by variable force: using integration6.02d Mechanical energy: KE and PE concepts6.02i Conservation of energy: mechanical energy principle6.06a Variable force: dv/dt or v*dv/dx methods

  1. A spacecraft \(S\) of mass \(m\) moves in a straight line towards the centre, \(O\), of a planet.
The planet is modelled as a fixed sphere of radius \(R\).
The spacecraft \(S\) is modelled as a particle.
The gravitational force of the planet is the only force acting on \(S\).
When \(S\) is a distance \(x ( x \geqslant R )\) from \(O\)
  • the gravitational force is directed towards \(O\) and has magnitude \(\frac { m g R ^ { 2 } } { 2 x ^ { 2 } }\)
  • the speed of \(S\) is \(v\)
    1. Show that
$$v ^ { 2 } = \frac { g R ^ { 2 } } { x } + C$$ where \(C\) is a constant. When \(x = 3 R , v = \sqrt { 3 g R }\)
  • Find, in terms of \(g\) and \(R\), the speed of \(S\) as it hits the surface of the planet.

  • Question 1:
    Part 1a:
    AnswerMarks Guidance
    Answer/WorkingMark Guidance
    \(-\dfrac{mgR^2}{2x^2} = mv\dfrac{\mathrm{d}v}{\mathrm{d}x}\)M1 Form differential equation in \(v\) and \(x\) only. Need to see \(\dfrac{\mathrm{d}v}{\mathrm{d}x}\) or \(v\dfrac{\mathrm{d}v}{\mathrm{d}x}\). Cannot get this mark using \(t\). Allow with both \(m\)'s cancelled. Condone sign error.
    \(-\dfrac{gR^2}{2}\int\dfrac{1}{x^2}\mathrm{d}x = \int v\mathrm{d}v\)M1 Separate variables correctly and integrate at least one side. Cannot get this mark using \(t\). Condone sign error.
    \(v^2 = \dfrac{gR^2}{x} + C\) *A1* Obtain given answer from correct work. Must include at least one line of working between integral and final answer. Correct signs seen throughout working. Condone \(\dfrac{v^2}{2} = \dfrac{gR^2}{2x} + C\) followed by \(v^2 = \dfrac{gR^2}{x} + C\). Note: If first line of working is \(\dfrac{1}{2}v^2 = -\int\dfrac{gR^2}{2x^2}\,\mathrm{d}x\) followed by integration of RHS, this scores M0M1A0*
    ALT1(a):
    AnswerMarks Guidance
    Answer/WorkingMark Guidance
    \(\dfrac{1}{2}mu^2 - \dfrac{1}{2}mv^2 = \int\dfrac{gmR^2}{x^2}\mathrm{d}x\)M1 Form an energy equation with 2 KE terms and the integral of the variable force. Condone sign errors.
    \(\dfrac{1}{2}mu^2 - \dfrac{1}{2}mv^2 = -\dfrac{gmR^2}{x} + A\)M1 Integrate the force wrt \(x\). Condone sign errors.
    \(v^2 = \dfrac{gR^2}{x} + C\) *A1* Obtain given answer from correct work. Must include at least one line of working and correct signs seen throughout working.
    [3]
    Part 1b:
    AnswerMarks Guidance
    Answer/WorkingMark Guidance
    \(x = 3R,\, v^2 = 3gR\)M1 Use initial conditions to evaluate \(C\) in the given answer.
    \(\Rightarrow C = 3gR - \dfrac{gR^2}{3R}\left(= \dfrac{8gR}{3}\right)\)A1 Or equivalent
    \(x = R \Rightarrow v = \sqrt{\dfrac{11gR}{3}}\)A1 Accept \(\dfrac{\sqrt{33gR}}{3}\). Answer must be in terms of \(g\) and \(R\).
    [3]
    ALT1(b):
    AnswerMarks Guidance
    Answer/WorkingMark Guidance
    \(\left[v^2\right]_{\sqrt{3gR}}^{v} = \left[\dfrac{gR^2}{x}\right]_{3R}^{R}\)M1 Use initial conditions in a definite integral.
    \(v^2 - 3gR = \dfrac{gR^2}{R} - \dfrac{gR^2}{3R}\)A1 Or equivalent
    \(v = \sqrt{\dfrac{11gR}{3}}\)A1 Accept \(\dfrac{\sqrt{33gR}}{3}\). Answer must be in terms of \(g\) and \(R\).
    [6] total
    # Question 1:
    
    ## Part 1a:
    
    | Answer/Working | Mark | Guidance |
    |---|---|---|
    | $-\dfrac{mgR^2}{2x^2} = mv\dfrac{\mathrm{d}v}{\mathrm{d}x}$ | M1 | Form differential equation in $v$ and $x$ only. Need to see $\dfrac{\mathrm{d}v}{\mathrm{d}x}$ or $v\dfrac{\mathrm{d}v}{\mathrm{d}x}$. Cannot get this mark using $t$. Allow with both $m$'s cancelled. Condone sign error. |
    | $-\dfrac{gR^2}{2}\int\dfrac{1}{x^2}\mathrm{d}x = \int v\mathrm{d}v$ | M1 | Separate variables correctly and integrate at least one side. Cannot get this mark using $t$. Condone sign error. |
    | $v^2 = \dfrac{gR^2}{x} + C$ * | A1* | Obtain given answer from correct work. Must include at least one line of working between integral and final answer. Correct signs seen throughout working. Condone $\dfrac{v^2}{2} = \dfrac{gR^2}{2x} + C$ followed by $v^2 = \dfrac{gR^2}{x} + C$. Note: If first line of working is $\dfrac{1}{2}v^2 = -\int\dfrac{gR^2}{2x^2}\,\mathrm{d}x$ followed by integration of RHS, this scores M0M1A0* |
    
    **ALT1(a):**
    
    | Answer/Working | Mark | Guidance |
    |---|---|---|
    | $\dfrac{1}{2}mu^2 - \dfrac{1}{2}mv^2 = \int\dfrac{gmR^2}{x^2}\mathrm{d}x$ | M1 | Form an energy equation with 2 KE terms and the integral of the variable force. Condone sign errors. |
    | $\dfrac{1}{2}mu^2 - \dfrac{1}{2}mv^2 = -\dfrac{gmR^2}{x} + A$ | M1 | Integrate the force wrt $x$. Condone sign errors. |
    | $v^2 = \dfrac{gR^2}{x} + C$ * | A1* | Obtain given answer from correct work. Must include at least one line of working and correct signs seen throughout working. |
    | | [3] | |
    
    ## Part 1b:
    
    | Answer/Working | Mark | Guidance |
    |---|---|---|
    | $x = 3R,\, v^2 = 3gR$ | M1 | Use initial conditions to evaluate $C$ in the given answer. |
    | $\Rightarrow C = 3gR - \dfrac{gR^2}{3R}\left(= \dfrac{8gR}{3}\right)$ | A1 | Or equivalent |
    | $x = R \Rightarrow v = \sqrt{\dfrac{11gR}{3}}$ | A1 | Accept $\dfrac{\sqrt{33gR}}{3}$. Answer must be in terms of $g$ and $R$. |
    | | [3] | |
    
    **ALT1(b):**
    
    | Answer/Working | Mark | Guidance |
    |---|---|---|
    | $\left[v^2\right]_{\sqrt{3gR}}^{v} = \left[\dfrac{gR^2}{x}\right]_{3R}^{R}$ | M1 | Use initial conditions in a definite integral. |
    | $v^2 - 3gR = \dfrac{gR^2}{R} - \dfrac{gR^2}{3R}$ | A1 | Or equivalent |
    | $v = \sqrt{\dfrac{11gR}{3}}$ | A1 | Accept $\dfrac{\sqrt{33gR}}{3}$. Answer must be in terms of $g$ and $R$. |
    | | [6] total | |
    
    ---
    \begin{enumerate}
      \item A spacecraft $S$ of mass $m$ moves in a straight line towards the centre, $O$, of a planet.
    \end{enumerate}
    
    The planet is modelled as a fixed sphere of radius $R$.\\
    The spacecraft $S$ is modelled as a particle.\\
    The gravitational force of the planet is the only force acting on $S$.\\
    When $S$ is a distance $x ( x \geqslant R )$ from $O$
    
    \begin{itemize}
      \item the gravitational force is directed towards $O$ and has magnitude $\frac { m g R ^ { 2 } } { 2 x ^ { 2 } }$
      \item the speed of $S$ is $v$\\
    (a) Show that
    \end{itemize}
    
    $$v ^ { 2 } = \frac { g R ^ { 2 } } { x } + C$$
    
    where $C$ is a constant.
    
    When $x = 3 R , v = \sqrt { 3 g R }$\\
    (b) Find, in terms of $g$ and $R$, the speed of $S$ as it hits the surface of the planet.
    
    \hfill \mbox{\textit{Edexcel M3 2024 Q1 [6]}}