Comprehensive assessment covering all of Module 5: projectile motion, circular motion, gravitational fields, orbital mechanics, and energy in orbits. This is a full module examination.
25 questions — select the best answer for each.
Questions 1–8 — IQ1
Q1. A projectile is launched at 25 m/s at 30° above the horizontal. What is the vertical component of its initial velocity?
Q2. A ball is kicked from level ground at 18 m/s, 45° above horizontal. How long is it in the air? ($g = 9.8 \text{ m/s}^2$)
Q3. A stone is thrown at 15 m/s, 60° above horizontal on Earth ($g = 9.8 \text{ m/s}^2$). What is its horizontal range?
Q4. What is the maximum height reached by a projectile launched at 30 m/s, 50° above horizontal? ($g = 9.8 \text{ m/s}^2$)
Q5. A ball is thrown horizontally at 12 m/s from a 45 m high cliff. How far horizontally does it travel before hitting the ground? ($g = 9.8 \text{ m/s}^2$, ignore air resistance)
Q6. Two projectiles are launched at the same speed from level ground. One at 30° has the same range as one launched at what other angle?
Q7. A projectile is launched on a planet where $g$ is half that of Earth. If launched at the same speed and angle, how do the range and maximum height compare?
Q8. The trajectory equation $y = x\tan\theta - \frac{gx^2}{2v^2\cos^2\theta}$ describes what shape?
Questions 9–17 — IQ2
Q9. A car drives around a circular track at constant speed. The direction of the centripetal acceleration is:
Q10. A 1200 kg car rounds a flat curve of radius 60 m at 20 m/s. What is the magnitude of the centripetal force required?
Q11. In a conical pendulum, what provides the horizontal component of tension that produces centripetal force?
Q12. A curve is banked at 15° with radius 100 m. What is the design speed? ($g = 9.8 \text{ m/s}^2$)
Q13. A 0.5 kg mass on a 1.2 m string swings in a vertical circle. What is the minimum speed at the top of the circle to maintain circular motion? ($g = 9.8 \text{ m/s}^2$)
Q14. A satellite orbits Earth at altitude 400 km. What is its orbital speed? ($M_E = 5.97 \times 10^{24} \text{ kg}$, $R_E = 6.37 \times 10^6 \text{ m}$, $G = 6.67 \times 10^{-11} \text{ N m}^2/\text{kg}^2$)
Q15. What is the approximate altitude of a geostationary orbit above Earth’s surface? ($M_E = 5.97 \times 10^{24} \text{ kg}$, $R_E = 6.37 \times 10^6 \text{ m}$)
Q16. A satellite in circular orbit has kinetic energy $KE$. What is its total mechanical energy?
Q17. What is the relationship between escape velocity $v_e$ and orbital velocity $v_o$ at the same radius?
Questions 18–25 — IQ3
Q18. Two 5.0 kg masses are placed 2.0 m apart. What is the gravitational force between them? ($G = 6.67 \times 10^{-11} \text{ N m}^2/\text{kg}^2$)
Q19. What is the gravitational field strength at an altitude of 2000 km above Earth’s surface? ($M_E = 5.97 \times 10^{24} \text{ kg}$, $R_E = 6.37 \times 10^6 \text{ m}$)
Q20. Which statement about gravitational potential energy $U = -GMm/r$ is correct?
Q21. How much work is required to move a 100 kg mass from Earth’s surface ($r = R_E$) to an altitude where $r = 2R_E$? ($g_0 = 9.8 \text{ m/s}^2$, $R_E = 6.37 \times 10^6 \text{ m}$)
Q22. The gravitational potential at a point in Earth’s field is $-40 \times 10^6 \text{ J/kg}$. What does this mean?
Q23. The relationship between gravitational field strength and gravitational potential is:
Q24. According to Kepler’s Third Law, if a planet’s orbital radius is doubled, its period becomes:
Q25. What is the Schwarzschild radius of a black hole with mass $3 \times 10^{31}$ kg? ($G = 6.67 \times 10^{-11} \text{ N m}^2/\text{kg}^2$, $c = 3.00 \times 10^8 \text{ m/s}$)
8 questions — show all working for full marks.
Questions 26–33 — working required
Q26. A ball is thrown at $20 \text{ m/s}$ at $40°$ above the horizontal from the top of a $30 \text{ m}$ high cliff. Find the horizontal range from the base of the cliff and the speed at which it hits the ground below. ($g = 9.8 \text{ m/s}^2$)
Q27. A $0.5 \text{ kg}$ bob on a $0.8 \text{ m}$ string makes 2 revolutions per second in a horizontal circle. Find the tension in the string and the angle the string makes with the vertical.
Q28. A $2000 \text{ kg}$ car rounds a banked curve of radius $80 \text{ m}$ banked at $12°$.
(a) Calculate the design speed at which no friction is required. ($g = 9.8 \text{ m/s}^2$)
(b) If $\mu_s = 0.30$, calculate the maximum speed the car can travel without slipping up the bank.
Q29. A satellite of mass $800 \text{ kg}$ orbits Earth at $r = 7.2 \times 10^6 \text{ m}$ from Earth’s centre. Calculate:
(a) the orbital speed $v$ and period $T$;
(b) the kinetic energy $KE$, gravitational potential energy $U$, and total energy $E$.
($M_E = 5.97 \times 10^{24} \text{ kg}$, $G = 6.67 \times 10^{-11} \text{ N m}^2/\text{kg}^2$)
Q30. Calculate the gravitational field strength at an altitude of $1500 \text{ km}$ above Earth’s surface. A $2.0 \text{ kg}$ mass is placed at this point — what is its weight? ($M_E = 5.97 \times 10^{24} \text{ kg}$, $R_E = 6.37 \times 10^6 \text{ m}$)
Q31. Find the minimum energy required to move a $1000 \text{ kg}$ satellite from Earth’s surface to an orbital radius of $1.0 \times 10^7 \text{ m}$. ($M_E = 5.97 \times 10^{24} \text{ kg}$, $R_E = 6.37 \times 10^6 \text{ m}$)
Q32. Starting from $V = -\dfrac{GM}{r}$, derive the relationship $g = -\dfrac{dV}{dr}$. Explain the physical meaning of the negative sign in this equation.
Q33. The star Proxima Centauri has mass $0.12\,M_{\odot}$ ($M_{\odot} = 1.99 \times 10^{30} \text{ kg}$). A planet orbits with period $11.2 \text{ days}$.
(a) Calculate the orbital radius of the planet.
(b) The habitable zone for this star is roughly $0.023\text{--}0.054 \text{ AU}$ ($1 \text{ AU} = 1.50 \times 10^{11} \text{ m}$). Assess whether liquid water could exist on this planet.
Q1: B — $v_y = v\sin\theta = 25 \times 0.5 = 12.5 \text{ m/s}$
Q2: C — $t = \frac{2 \times 18 \times \sin 45°}{9.8} = 2.60 \text{ s}$
Q3: B — $R = \frac{15^2 \times \sin 120°}{9.8} = 19.9 \text{ m}$
Q4: B — $H_{\max} = \frac{30^2 \times \sin^2 50°}{2 \times 9.8} = 27.0 \text{ m}$
Q5: A — $t = \sqrt{\frac{2 \times 45}{9.8}} = 3.03 \text{ s}$; $x = 12 \times 3.03 = 36.4 \text{ m}$
Q6: C — Complementary angles: $90° - 30° = 60°$
Q7: C — Both $R$ and $H_{\max}$ are inversely proportional to $g$
Q8: B — Quadratic in $x$ describes a parabola
Q9: B — Centripetal acceleration always points toward the centre
Q10: B — $F_c = \frac{1200 \times 20^2}{60} = 8000 \text{ N}$
Q11: B — Horizontal component of tension provides $F_c$
Q12: B — $v = \sqrt{100 \times 9.8 \times \tan 15°} = 16.2 \text{ m/s}$
Q13: A — $v_{\min} = \sqrt{gr} = \sqrt{9.8 \times 1.2} = 3.43 \text{ m/s}$
Q14: C — $v = \sqrt{\frac{GM}{6.77 \times 10^6}} = 7.67 \text{ km/s}$
Q15: C — Geostationary altitude $\approx 35\,800 \text{ km}$
Q16: B — $E = KE + U = KE - 2KE = -KE$
Q17: C — $v_e = \sqrt{2GM/r} = \sqrt{2}\,v_o$
Q18: B — $F = \frac{6.67 \times 10^{-11} \times 25}{4} = 4.17 \times 10^{-10} \text{ N}$
Q19: A — $g = \frac{GM}{(8.37 \times 10^6)^2} = 5.69 \text{ m/s}^2$
Q20: B — Negative sign indicates binding, attractive force
Q21: B — $W = mg_0R_E/2 = 3.13 \times 10^9 \text{ J}$
Q22: C — Work against field to reach infinity = $40 \times 10^6$ J/kg
Q23: A — $g = -dV/dr$ (negative potential gradient)
Q24: B — $T \propto r^{3/2}$, so $T \to 2^{3/2}T = 2\sqrt{2}\,T$
Q25: C — $R_s = \frac{2GM}{c^2} = 4.45 \times 10^4 \text{ m}$
Given: $v = 20 \text{ m/s}$, $\theta = 40°$, $h = 30 \text{ m}$, $g = 9.8 \text{ m/s}^2$
$v_x = 20\cos 40° = 15.32 \text{ m/s}$; $v_y = 20\sin 40° = 12.86 \text{ m/s}$ (upward)
Fall time: Downward displacement is $-30$ m. Using $s = ut + \frac{1}{2}at^2$:
$-30 = 12.86t - 4.9t^2 \Rightarrow 4.9t^2 - 12.86t - 30 = 0$
$t = \frac{12.86 + \sqrt{12.86^2 + 4 \times 4.9 \times 30}}{9.8} = \frac{12.86 + 19.42}{9.8} = 3.29 \text{ s}$ (1 mark)
Range: $x = v_x t = 15.32 \times 3.29 = \mathbf{50.4 \text{ m}}$ (1 mark)
Impact speed: $v_y(\text{final}) = 12.86 - 9.8 \times 3.29 = -19.38 \text{ m/s}$
$v = \sqrt{15.32^2 + (-19.38)^2} = \sqrt{234.7 + 375.6} = \sqrt{610.3} = \mathbf{24.7 \text{ m/s}}$ (1 mark)
Given: $m = 0.5 \text{ kg}$, $L = 0.8 \text{ m}$, $f = 2 \text{ Hz}$, $\omega = 2\pi f = 4\pi = 12.57 \text{ rad/s}$
Radius of horizontal circle: $r = L\sin\theta$
Vertical: $T\cos\theta = mg$; Horizontal: $T\sin\theta = m\omega^2 r = m\omega^2 L\sin\theta$
From horizontal: $T = m\omega^2 L = 0.5 \times (12.57)^2 \times 0.8 = 0.5 \times 157.9 \times 0.8 = \mathbf{63.2 \text{ N}}$ (1 mark)
From vertical: $\cos\theta = \frac{mg}{T} = \frac{0.5 \times 9.8}{63.2} = \frac{4.9}{63.2} = 0.0775$
$\theta = \cos^{-1}(0.0775) = \mathbf{85.6°}$ (1 mark for method, 1 mark for answer)
(a) Design speed (2 marks):
$v_d = \sqrt{rg\tan\theta} = \sqrt{80 \times 9.8 \times \tan 12°} = \sqrt{80 \times 9.8 \times 0.2126}$
$v_d = \sqrt{166.7} = \mathbf{12.9 \text{ m/s}}$ ($\approx 46.5 \text{ km/h}$)
(b) Maximum speed with friction (2 marks):
At maximum speed, friction acts down the slope. Resolving:
$N\cos\theta = mg + \mu_s N\sin\theta$ and $N\sin\theta + \mu_s N\cos\theta = \frac{mv^2}{r}$
$v_{\max}^2 = rg\left(\frac{\tan\theta + \mu_s}{1 - \mu_s\tan\theta}\right) = 80 \times 9.8 \times \left(\frac{0.2126 + 0.30}{1 - 0.30 \times 0.2126}\right)$
$v_{\max}^2 = 784 \times \frac{0.5126}{0.9362} = 784 \times 0.5475 = 429.2$
$v_{\max} = \sqrt{429.2} = \mathbf{20.7 \text{ m/s}}$ ($\approx 74.5 \text{ km/h}$)
(a) Orbital speed and period (2 marks):
$v = \sqrt{\frac{GM}{r}} = \sqrt{\frac{6.67 \times 10^{-11} \times 5.97 \times 10^{24}}{7.2 \times 10^6}} = \sqrt{\frac{3.98 \times 10^{14}}{7.2 \times 10^6}} = \sqrt{5.53 \times 10^7}$
$v = \mathbf{7.43 \times 10^3 \text{ m/s}}$ ($7.43 \text{ km/s}$)
$T = \frac{2\pi r}{v} = \frac{2\pi \times 7.2 \times 10^6}{7.43 \times 10^3} = \mathbf{6.09 \times 10^3 \text{ s} = 101.5 \text{ min}}$
(b) Energies (2 marks):
$KE = \frac{1}{2}mv^2 = 0.5 \times 800 \times (7.43 \times 10^3)^2 = \mathbf{2.21 \times 10^{10} \text{ J}}$
$U = -\frac{GMm}{r} = -\frac{6.67 \times 10^{-11} \times 5.97 \times 10^{24} \times 800}{7.2 \times 10^6} = \mathbf{-4.42 \times 10^{10} \text{ J}}$
$E = KE + U = 2.21 \times 10^{10} - 4.42 \times 10^{10} = \mathbf{-2.21 \times 10^{10} \text{ J}}$
Note: $E = -KE$ and $U = -2KE$ as expected for a circular orbit.
$r = R_E + h = 6.37 \times 10^6 + 1.50 \times 10^6 = 7.87 \times 10^6 \text{ m}$ (1 mark)
$g = \frac{GM}{r^2} = \frac{6.67 \times 10^{-11} \times 5.97 \times 10^{24}}{(7.87 \times 10^6)^2} = \frac{3.98 \times 10^{14}}{6.19 \times 10^{13}}$
$g = \mathbf{6.43 \text{ m/s}^2}$ (1 mark)
$W = mg = 2.0 \times 6.43 = \mathbf{12.9 \text{ N}}$ (1 mark)
Note: Weight is $\approx 31\%$ less than at the surface ($19.6 \text{ N}$), showing $g$ decreases with altitude.
$W = \Delta U = GMm\left(\frac{1}{R_E} - \frac{1}{r_2}\right)$ (1 mark for formula)
$W = 6.67 \times 10^{-11} \times 5.97 \times 10^{24} \times 1000 \times \left(\frac{1}{6.37 \times 10^6} - \frac{1}{1.0 \times 10^7}\right)$
$W = 3.98 \times 10^{17} \times (1.570 \times 10^{-7} - 1.000 \times 10^{-7})$
$W = 3.98 \times 10^{17} \times 5.70 \times 10^{-8} = \mathbf{2.27 \times 10^{10} \text{ J}}$ (2 marks)
Alternatively: $W = mg_0R_E^2(\frac{1}{R_E} - \frac{1}{r_2}) = 1000 \times 9.8 \times (6.37 \times 10^6)^2 \times 5.70 \times 10^{-8}$
Derivation (2 marks):
Starting with $V = -\dfrac{GM}{r} = -GMr^{-1}$
$\dfrac{dV}{dr} = -GM \times (-1)r^{-2} = \dfrac{GM}{r^2}$
Since $g = \dfrac{GM}{r^2}$, we have $\dfrac{dV}{dr} = g$
Therefore $\mathbf{g = -\dfrac{dV}{dr}}$
Physical meaning (2 marks):
The gravitational field $g$ points in the direction of decreasing potential (toward the mass). Since potential increases with $r$ (becomes less negative), $\frac{dV}{dr} > 0$, so the negative sign ensures $g$ points inward (radially inward). The negative sign tells us that the field is directed toward regions of lower potential energy.
(a) Orbital radius (2 marks):
$M = 0.12 \times 1.99 \times 10^{30} = 2.39 \times 10^{29} \text{ kg}$
$T = 11.2 \text{ days} = 11.2 \times 24 \times 3600 = 9.68 \times 10^5 \text{ s}$
From Kepler’s Third Law: $r^3 = \dfrac{GMT^2}{4\pi^2}$
$r^3 = \dfrac{6.67 \times 10^{-11} \times 2.39 \times 10^{29} \times (9.68 \times 10^5)^2}{4\pi^2}$
$r^3 = \dfrac{1.50 \times 10^{29}}{39.48} = 3.80 \times 10^{27}$
$r = \sqrt[3]{3.80 \times 10^{27}} = \mathbf{1.56 \times 10^9 \text{ m}}$ (1.56 million km)
In AU: $r = \frac{1.56 \times 10^9}{1.50 \times 10^{11}} = \mathbf{0.0104 \text{ AU}}$
(b) Assessment (2 marks):
The planet orbits at $0.0104 \text{ AU}$, which is inside the habitable zone of $0.023\text{--}0.054 \text{ AU}$. (1 mark)
Since it orbits closer than the inner edge of the habitable zone, the planet would likely be too hot for liquid water to exist on its surface. It would receive significantly more stellar flux than Earth, making surface temperatures high enough to boil water. Therefore, liquid water is unlikely to exist on this planet. (1 mark for reasoned conclusion)
I have completed this full module assessment and reviewed my answers.