What is the single hardest thing about projectile motion problems? What will you focus on improving?
No new content. Six formulae. Six common errors. Ten mixed practice questions. Three timed extended responses. This is your Phase 1 exam preparation.
Click each card to reveal when to use it, common traps, and connections.
Phase1 Summary
Each card shows a student's incorrect working. Find the error, explain the fix, then check.
Ten questions from Band 3 to Band 6. Worked solutions in the Answers section below.
Three exam-style questions. Each: 4 marks, 8 minutes recommended. Solutions in the Answers section.
After working through the practice questions, reflect again:
1. A projectile is launched at 20 m/s, 60° above horizontal. What is the initial vertical component of velocity?
2. At the maximum height of a projectile's trajectory, which statement is true?
3. The range formula $R = \frac{v^2\sin(2\theta)}{g}$ can only be used when:
4. A projectile is launched horizontally from a height $h$ with speed $v$. Which change would double the horizontal range?
5. Two projectiles are launched at the same speed on level ground: P at 30° and Q at 60°. Which statement is correct?
1. A student claims that increasing the launch angle of a projectile always increases its range. Assess this claim with reference to the range formula and specific angles.
2. A ball is thrown at 16 m/s at an angle of 40° above horizontal. Calculate the horizontal and vertical components of velocity, the time to reach maximum height, and the maximum height above the launch point.
3. Evaluate the statement: "The time of flight of a projectile depends only on its vertical component of velocity and is independent of the horizontal component." Use equations and a numerical example to justify your answer.
$v_x = v\cos\theta = 12\cos 40° = \mathbf{9.19 \text{ m/s}}$ (1 mark)
$v_y = v\sin\theta = 12\sin 40° = \mathbf{7.71 \text{ m/s}}$ (1 mark)
(a) Vertical: $s_y = \frac{1}{2}gt^2$ so $t = \sqrt{\frac{2s_y}{g}} = \sqrt{\frac{2 \times 40}{9.8}} = \mathbf{2.86 \text{ s}}$ (1 mark)
(b) Horizontal: $s_x = v_x t = 15 \times 2.86 = \mathbf{42.9 \text{ m}}$ (1 mark)
Any two of: (1) No air resistance / negligible air resistance; (2) Acceleration due to gravity is constant ($g = 9.8$ m s² downward); (3) Launch and landing heights are the same (level ground); (4) Earth is flat over the trajectory (g is uniform, not radial). (1 mark each)
$u_y = 22\sin 35° = 12.62$ m/s; $v_x = 22\cos 35° = 18.02$ m/s
(a) $h_{\max} = \frac{u_y^2}{2g} = \frac{12.62^2}{2 \times 9.8} = \mathbf{8.13 \text{ m}}$ (1 mark)
(b) $t_{\text{flight}} = \frac{2u_y}{g} = \frac{2 \times 12.62}{9.8} = \mathbf{2.58 \text{ s}}$ (1 mark)
(c) $R = v_x \times t = 18.02 \times 2.58 = \mathbf{46.5 \text{ m}}$ (1 mark)
Or use $R = \frac{v^2\sin(2\theta)}{g} = \frac{22^2 \times \sin 70°}{9.8} = 46.5$ m
$u_y = 18\sin 30° = 9.0$ m/s; $v_x = 18\cos 30° = 15.59$ m/s
Vertical: $s_y = u_y t + \frac{1}{2}at^2$ with $s_y = -25$ m (downward positive convention or $a = -9.8$ with up positive):
$-25 = 9.0t + \frac{1}{2}(-9.8)t^2$ → $-25 = 9.0t - 4.9t^2$
$4.9t^2 - 9.0t - 25 = 0$
Using quadratic formula: $t = \frac{9.0 + \sqrt{81 + 490}}{9.8} = \frac{9.0 + 23.85}{9.8} = \mathbf{3.35 \text{ s}}$ (positive root) (2 marks for method + time)
Horizontal: $s_x = 15.59 \times 3.35 = \mathbf{52.2 \text{ m}}$ (1 mark)
For θ = 20°: $R_1 = \frac{v^2\sin(40°)}{g}$ (1 mark)
For θ = 70°: $R_2 = \frac{v^2\sin(140°)}{g}$ (1 mark)
Since $\sin(140°) = \sin(180° - 40°) = \sin(40°)$, we have $R_1 = R_2$. (1 mark)
Key identity: $\sin(2\theta) = \sin(180° - 2\theta)$, so angles θ and $(90° - \theta)$ give the same range.
At the wall: $s_x = 15$ m, $s_y = 5$ m, θ = 25°.
$s_x = v\cos\theta \cdot t$ → $t = \frac{15}{v\cos 25°}$ (1 mark)
$s_y = v\sin\theta \cdot t - \frac{1}{2}gt^2$
$5 = v\sin 25° \cdot \frac{15}{v\cos 25°} - 4.9\left(\frac{15}{v\cos 25°}\right)^2$
$5 = 15\tan 25° - \frac{4.9 \times 225}{v^2\cos^2 25°}$
$5 = 6.99 - \frac{1102.5}{v^2 \times 0.821}$
$\frac{1102.5}{0.821v^2} = 6.99 - 5 = 1.99$ (1 mark)
$v^2 = \frac{1102.5}{0.821 \times 1.99} = 675$ → $v = \mathbf{26.0 \text{ m/s}}$ (2 marks)
Given: launch height = 1.5 m, basket at 20 m horizontal, 3.0 m height. So $\Delta s_x = 20$ m, $\Delta s_y = +1.5$ m.
$s_x = v\cos\theta \cdot t = 20$ ... (1)
$s_y = v\sin\theta \cdot t - 4.9t^2 = 1.5$ ... (2) (1 mark)
From (1): $v\cos\theta = \frac{20}{t}$. From (2): $v\sin\theta = \frac{1.5 + 4.9t^2}{t}$
$\tan\theta = \frac{v\sin\theta}{v\cos\theta} = \frac{1.5 + 4.9t^2}{20}$ (1 mark)
Also $v^2 = (v\cos\theta)^2 + (v\sin\theta)^2 = \frac{400}{t^2} + \frac{(1.5 + 4.9t^2)^2}{t^2}$
By trial or solving: try $t = 1.5$ s: $\tan\theta = \frac{1.5 + 11.0}{20} = 0.625$ → θ = 32.0°.
$v = \frac{20}{1.5\cos 32°} = \frac{20}{1.27} = 15.7$ m/s. Check: $s_y = 15.7\sin 32° \times 1.5 - 4.9(1.5)^2 = 8.32 \times 1.5 - 11.0 = 12.5 - 11.0 = 1.5$ m ✓ (2 marks)
θ ≈ 32°, v ≈ 15.7 m/s (accept reasonable ranges from rounding).
Given: same speed $v$, A at 30°, B at 60°.
Maximum height: $h \propto \sin^2\theta$. $\sin^2 60° = 0.75$, $\sin^2 30° = 0.25$. So B reaches 3× the height of A. (1 mark)
Flight time: $t \propto \sin\theta$. $\sin 60° = 0.866$, $\sin 30° = 0.5$. So B stays in the air 1.73× longer than A. (1 mark)
Range: $R \propto \sin(2\theta)$. $\sin 60° = \sin 120° = \frac{\sqrt{3}}{2}$. Same range. (1 mark)
Explanation: 30° and 60° are complementary angles. The smaller angle gives less vertical velocity (shorter time, lower height) but more horizontal velocity. The larger angle gives more vertical velocity (longer time, greater height) but less horizontal velocity. These two effects exactly balance for range because $\sin(2\theta)$ is symmetric about 45°. (1 mark)
Let time to max height = $t_1$, time from explosion to landing = $t_2$, total time = 4.5 s.
At max height: spark travels horizontally at 5 m/s. Horizontal distance from explosion point = $5t_2$.
Total horizontal distance from launch = $v\cos\theta \cdot t_1 + 5 \cdot t_2 = 45$ m ... (1) (1 mark)
Time to max height: $t_1 = \frac{v\sin\theta}{g}$. Explosion height: $h = \frac{(v\sin\theta)^2}{2g}$.
Fall time from height $h$: $h = \frac{1}{2}gt_2^2$ so $t_2 = \sqrt{\frac{2h}{g}} = \frac{v\sin\theta}{g} = t_1$. (1 mark)
So $t_1 = t_2 = \frac{4.5}{2} = 2.25$ s. (1 mark)
From $t_1 = \frac{v\sin\theta}{g}$: $v\sin\theta = 9.8 \times 2.25 = 22.05$ m/s.
From (1): $v\cos\theta \times 2.25 + 5 \times 2.25 = 45$ → $2.25(v\cos\theta + 5) = 45$
$v\cos\theta + 5 = 20$ → $v\cos\theta = 15$ m/s. (1 mark)
$v = \sqrt{(v\sin\theta)^2 + (v\cos\theta)^2} = \sqrt{22.05^2 + 15^2} = \sqrt{486.2 + 225} = \sqrt{711.2} = \mathbf{26.7 \text{ m/s}}$
$\tan\theta = \frac{22.05}{15} = 1.47$ → $\theta = \mathbf{55.8°}$ (1 mark)
(a) $v_x = 9.2\cos 22° = \mathbf{8.53 \text{ m/s}}$; $u_y = 9.2\sin 22° = \mathbf{3.45 \text{ m/s}}$ (1 mark)
(b) $t = \frac{2u_y}{g} = \frac{2 \times 3.45}{9.8} = \mathbf{0.704 \text{ s}}$ (1 mark)
(c) $R = v_x \times t = 8.53 \times 0.704 = \mathbf{6.01 \text{ m}}$ (1 mark)
(d) $h_{\max} = \frac{u_y^2}{2g} = \frac{3.45^2}{19.6} = \mathbf{0.607 \text{ m}}$ (1 mark)
$v_x = 15\cos 50° = 9.64$ m/s; $u_y = 15\sin 50° = 11.49$ m/s
(a) Time to max height: $t_{up} = \frac{u_y}{g} = \frac{11.49}{9.8} = \mathbf{1.17 \text{ s}}$ (1 mark)
(b) For total flight: $s_y = -30$ m (down). $-30 = 11.49t - 4.9t^2$ → $4.9t^2 - 11.49t - 30 = 0$
$t = \frac{11.49 + \sqrt{132.0 + 588}}{9.8} = \frac{11.49 + 26.93}{9.8} = \mathbf{3.92 \text{ s}}$ (1 mark)
(c) $s_x = 9.64 \times 3.92 = \mathbf{37.8 \text{ m}}$ (1 mark)
(d) At impact: $v_x = 9.64$ m/s (constant). $v_y = u_y - gt = 11.49 - 9.8(3.92) = 11.49 - 38.4 = -26.9$ m/s.
$v = \sqrt{9.64^2 + 26.9^2} = \mathbf{28.6 \text{ m/s}}$. Direction: $\tan\theta = \frac{26.9}{9.64}$ below horizontal, θ = 70.3°. (1 mark)
(a) $R = \frac{v^2\sin(2\theta)}{g}$ → $72 = \frac{30^2 \sin(2\theta)}{9.8}$
$\sin(2\theta) = \frac{72 \times 9.8}{900} = 0.784$ (1 mark)
$2\theta = \sin^{-1}(0.784) = 51.6°$ or $180° - 51.6° = 128.4°$
$\theta = \mathbf{25.8°}$ or $\mathbf{64.2°}$ (1 mark)
(b) For θ = 25.8°: $t = \frac{2 \times 30 \times \sin 25.8°}{9.8} = \frac{60 \times 0.435}{9.8} = \mathbf{2.66 \text{ s}}$
For θ = 64.2°: $t = \frac{2 \times 30 \times \sin 64.2°}{9.8} = \frac{60 \times 0.901}{9.8} = \mathbf{5.52 \text{ s}}$ (1 mark)
(c) There are two angles because $\sin(2\theta)$ has the same value for $2\theta$ and $(180° - 2\theta)$. The lower angle gives a smaller vertical component (shorter time, lower max height) but larger horizontal component. The higher angle gives a larger vertical component (longer time, greater max height) but smaller horizontal component. These two combinations produce the same range because the extra flight time of the high angle exactly compensates for the reduced horizontal speed. (1 mark)
1. B ($20\sin 60° = 17.3$ m/s)
2. C (At max height, $v_y = 0$ only)
3. B (Launch = landing height required)
4. A (Doubling $v$ doubles $R$ since $R \propto v$)
5. B (30° and 60° are complementary → same range)
The claim is incorrect. From $R = \frac{v^2\sin(2\theta)}{g}$, range depends on $\sin(2\theta)$, which is maximum at $\theta = 45°$. (1 mark) Increasing the angle from, say, 30° to 45° does increase range. But increasing beyond 45° decreases range because $\sin(2\theta)$ decreases. (1 mark) For example, $\sin(60°) = 0.866$ at 30° and $\sin(90°) = 1.0$ at 45°, but $\sin(120°) = 0.866$ at 60° — same range as 30°. So range increases up to 45° then decreases. (1 mark)
$v_x = 16\cos 40° = \mathbf{12.3 \text{ m/s}}$; $u_y = 16\sin 40° = \mathbf{10.3 \text{ m/s}}$ (1 mark)
$t_{up} = \frac{u_y}{g} = \frac{10.3}{9.8} = \mathbf{1.05 \text{ s}}$ (1 mark)
$h_{\max} = \frac{u_y^2}{2g} = \frac{10.3^2}{19.6} = \mathbf{5.41 \text{ m}}$ (1 mark)
The statement is correct. (1 mark) The flight time is found from vertical motion only. For level ground: $t = \frac{2v\sin\theta}{g} = \frac{2u_y}{g}$, which depends only on $u_y$, the vertical component. (1 mark) The horizontal component $v_x = v\cos\theta$ does not appear in the flight time equation. Numerical example: launch at 20 m/s at 30° vs 60°. Same $v$, different flight times: $t_{30} = \frac{2 \times 20 \times 0.5}{9.8} = 2.04$ s; $t_{60} = \frac{2 \times 20 \times 0.866}{9.8} = 3.54$ s. The horizontal component changed (17.3 m/s vs 10 m/s) but flight time changed because the vertical component changed, not the horizontal. (1 mark) Even if $v_x$ were zero (straight up), time depends only on $u_y$. If $v_x$ doubled while $u_y$ stayed the same, flight time would not change. (1 mark)
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