Test the prescribed core from Lessons 6–8 and 10–12: torque, uniform circular motion, banked curves, gravitation, orbital mechanics and energy in circular orbits. Lesson 9 vertical circles are optional extension and are not scored here.
Select the best answer for each question. Feedback appears after you choose.
Q1. A car moves around a circular track at constant speed. Which statement is correct?
Q2. A particle moves in a circle of radius 2.0 m with angular velocity $4.0\text{ rad s}^{-1}$. What is its centripetal acceleration?
Q3. A 0.50 kg mass is attached to a string and whirled in a horizontal circle of radius 0.80 m at $3.0\text{ m s}^{-1}$. What is the tension in the string?
Q4. A satellite completes one orbit every 90 minutes. What is its angular velocity in $\text{rad s}^{-1}$?
Q5. A mechanic applies a 60 N force to a wrench of length 0.30 m at an angle of 30° to the wrench handle. What is the torque applied to the nut?
Q6. A uniform seesaw is balanced horizontally with a 30 kg child sitting 2.0 m from the pivot on one side. Where must a 40 kg child sit on the other side to maintain balance?
Q7. In a conical pendulum, what provides the centripetal force?
Q8. A conical pendulum makes an angle $\theta$ with the vertical. Which relationship is correct?
Q9. A curve of radius 50 m is banked at $15^{\circ}$. What is the design speed at which no friction is needed? ($g = 9.8\text{ m s}^{-2}$)
Q10. A car travels faster than the design speed on a banked curve. What happens?
Q11. Why does the radial net force do zero work on an object in ideal uniform circular motion?
Q12. An object moves in a circle at twice its original speed while mass and radius remain constant. The required radial net force becomes:
Q13. A satellite orbits Earth at altitude $h$. Which expression gives the correct orbital speed? ($R_E$ = Earth's radius)
Q14. Two satellites orbit the same planet. Satellite A has orbital radius $r$ and period $T$. Satellite B has orbital radius $4r$. What is the period of satellite B?
Q15. Which of the following correctly describes the total mechanical energy of a satellite in a stable circular orbit?
Q16. A geostationary satellite must satisfy which condition?
Q17. Optional preview of Lesson 16, not part of the core score. The escape speed from a planet depends on which factors?
Show all working. Marks are awarded for correct method, substitution, and final answer with units.
Q1. A 1200 kg car travels around a 35 m radius curve at 18 m/s. Calculate the centripetal acceleration and the friction force required. Explain what happens if the road is icy. 3 marks
Q2. A conical pendulum has a 0.4 kg bob on a 0.6 m string making $30^{\circ}$ with the vertical. Calculate the tension in the string and the period of motion. 3 marks
Q3. A student holds mass at $0.50\text{ kg}$ and radius at $0.80\text{ m}$, then records radial force at speeds of $2.0$, $3.0$ and $4.0\text{ m s}^{-1}$ as $2.5$, $5.6$ and $10.0\text{ N}$. Identify a graph that linearises the data, state its predicted gradient, and evaluate whether the data support the model $F_c=mv^2/r$. 4 marks
Q4. A satellite orbits Earth at altitude 800 km. Calculate its orbital speed, period, and total energy (mass = 500 kg). Use $G = 6.67 \times 10^{-11}\text{ N m}^2\text{ kg}^{-2}$, $M_E = 5.97 \times 10^{24}\text{ kg}$, $R_E = 6.37 \times 10^6\text{ m}$. 4 marks
Q5. Optional L16 preview. Derive the escape-speed formula $v_e = \sqrt{2GM/r}$ from energy conservation principles. Explain why the factor of 2 appears and why escape speed is independent of the projectile's mass. This preview does not count toward L06–L12 core mastery. 4 marks
Q1: B, The car is accelerating because the direction of its velocity is continuously changing.
Q2: C, $a_c = \omega^2 r = (4.0)^2 \times 2.0 = 32\text{ m s}^{-2}$
Q3: C, $T = mv^2/r = (0.50)(3.0)^2/(0.80) = 5.6\text{ N}$
Q4: B, $\omega = 2\pi/T = 2\pi/(90 \times 60) = 2\pi/5400 = 1.16 \times 10^{-3}\text{ rad s}^{-1}$
Q5: A, $\tau=rF\sin\theta=(0.30)(60)\sin30^\circ=9.0\text{ N m}$
Q6: C, rotational equilibrium gives $(30)(2.0)=(40)r$, so $r=1.5\text{ m}$
Q7: B, the horizontal component of tension provides the radial resultant
Q8: A, $\tan\theta=v^2/(rg)$
Q9: B, $v=\sqrt{rg\tan\theta}=11.5\text{ m s}^{-1}$
Q10: B, friction acts down the slope when the car is faster than design speed
Q11: C, radial force is perpendicular to instantaneous displacement
Q12: C, doubling speed makes $F_c$ four times as large
Q13: B, $v=\sqrt{GM_E/(R_E+h)}$ uses centre-to-centre distance
Q14: C, $T_B=8T$ from $T^2\propto r^3$
Q15: C, total energy is $-GMm/(2r)$ for a circular orbit
Q16: B, equatorial orbit with a 24-hour period in Earth's rotation direction
Q17: B, escape speed depends on central mass and radial distance, not projectile mass
Given: $m = 1200\text{ kg}$, $r = 35\text{ m}$, $v = 18\text{ m s}^{-1}$
Centripetal acceleration:
$a_c = \dfrac{v^2}{r} = \dfrac{(18)^2}{35} = \dfrac{324}{35} = \mathbf{9.26\text{ m s}^{-2}}$
Friction force (provides centripetal force):
$F_f = F_c = \dfrac{mv^2}{r} = ma_c = 1200 \times 9.26 = \mathbf{1.11 \times 10^4\text{ N}}$
(or $F_f = 1200 \times 324/35 = 11109 \approx 1.1 \times 10^4\text{ N}$)
If the road is icy: The friction force is greatly reduced. If $F_{f,\text{max}} < mv^2/r$, the car cannot maintain the circular path and will skid outward (continue in a straight line tangent to the curve), this is not due to a fictitious "centrifugal force" but because friction is insufficient to provide the required centripetal force.
Given: $m = 0.4\text{ kg}$, $L = 0.6\text{ m}$, $\theta = 30^{\circ}$
Tension: Resolve vertically: $T\cos\theta = mg$
$T = \dfrac{mg}{\cos\theta} = \dfrac{0.4 \times 9.8}{\cos 30^{\circ}} = \dfrac{3.92}{0.866} = \mathbf{4.53\text{ N}}$
Period: The radius of the horizontal circle is $r = L\sin\theta = 0.6 \times \sin 30^{\circ} = 0.30\text{ m}$.
From $\tan\theta = v^2/(rg)$: $v = \sqrt{rg\tan\theta} = \sqrt{0.30 \times 9.8 \times \tan 30^{\circ}} = \sqrt{0.30 \times 9.8 \times 0.577} = \sqrt{1.70} = 1.30\text{ m s}^{-1}$
Period: $T = \dfrac{2\pi r}{v} = \dfrac{2\pi \times 0.30}{1.30} = \mathbf{1.45\text{ s}}$
Alternative method: $T = 2\pi\sqrt{\dfrac{L\cos\theta}{g}} = 2\pi\sqrt{\dfrac{0.6 \times 0.866}{9.8}} = 2\pi\sqrt{0.053} = 1.45\text{ s}$
Plot $F_c$ on the vertical axis against $v^2$ on the horizontal axis (1 mark). Since $F_c=(m/r)v^2$, the predicted gradient is $m/r=0.50/0.80=\mathbf{0.625\text{ kg m}^{-1}}$; equivalently the graph's units are $\text{N}/(\text{m}^2\text{s}^{-2})$ (1 mark).
The three $v^2$ values are $4.0$, $9.0$ and $16.0\text{ m}^2\text{s}^{-2}$. Multiplying each by $0.625$ predicts $2.50$, $5.625$ and $10.0\text{ N}$, which agree with the recorded values after rounding (1 mark). The data therefore support the squared-speed relationship within the precision supplied, but because they are model/simulated values with no independent uncertainty, they demonstrate consistency rather than validating a physical apparatus (1 mark).
Given: $h = 800\text{ km} = 8.0 \times 10^5\text{ m}$, $m = 500\text{ kg}$, $R_E = 6.37 \times 10^6\text{ m}$
Centre-to-centre distance: $r = R_E + h = 6.37 \times 10^6 + 0.80 \times 10^6 = \mathbf{7.17 \times 10^6\text{ m}}$
Orbital speed:
$v = \sqrt{\dfrac{GM_E}{r}} = \sqrt{\dfrac{6.67 \times 10^{-11} \times 5.97 \times 10^{24}}{7.17 \times 10^6}}$
$v = \sqrt{\dfrac{3.982 \times 10^{14}}{7.17 \times 10^6}} = \sqrt{5.554 \times 10^7} = \mathbf{7.45 \times 10^3\text{ m s}^{-1}}$ (or $7.45\text{ km s}^{-1}$)
Period:
$T = \dfrac{2\pi r}{v} = \dfrac{2\pi \times 7.17 \times 10^6}{7.45 \times 10^3} = \mathbf{6.05 \times 10^3\text{ s}} = \mathbf{101\text{ min}}$
Total energy:
$E = -\dfrac{GM_E m}{2r} = -\dfrac{6.67 \times 10^{-11} \times 5.97 \times 10^{24} \times 500}{2 \times 7.17 \times 10^6}$
$E = -\dfrac{1.991 \times 10^{17}}{1.434 \times 10^7} = \mathbf{-1.39 \times 10^{10}\text{ J}}$
(Negative, indicating a bound orbit.)
Derivation:
For an object to escape a planet's gravitational field, its total mechanical energy must be at least zero (so it can reach infinity with zero or positive kinetic energy).
At the surface (distance $r$ from centre):
$E = KE + U = \dfrac{1}{2}mv_e^2 + \left(-\dfrac{GMm}{r}\right) = 0$
For minimum escape: $\dfrac{1}{2}mv_e^2 = \dfrac{GMm}{r}$
Solving for $v_e$: $v_e^2 = \dfrac{2GM}{r}$
$\boxed{v_e = \sqrt{\dfrac{2GM}{r}}}$
Why the factor of 2 appears:
The factor of 2 arises because the kinetic energy needed must equal the magnitude of the gravitational potential energy at the launch point. Since $U = -GMm/r$, we need $KE = +GMm/r$ to bring total energy to zero. The kinetic energy formula has a factor of $\frac{1}{2}$, so when we equate $\frac{1}{2}mv^2$ with $GMm/r$, the 2 appears in the numerator of the final expression.
Why escape velocity is independent of projectile mass:
The mass $m$ of the projectile appears on both sides of the energy equation: $\frac{1}{2}mv_e^2 = GMm/r$. Dividing both sides by $m$, it cancels completely. This means any object, regardless of its mass, needs the same initial speed to escape from a given distance $r$. A feather and a rocket require the same $v_e$ (though the rocket has much more kinetic energy due to its larger mass).
Track your progress through Module 5.