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Formulas/physics/Kinematics/Range of a Projectile

Range of a Projectile

Horizontal range on level ground. Maximum range at θ = 45°.
Class 11Class JEE
Derivation

What this formula says

A projectile is launched from the ground with speed uu at angle θ\theta. It lands back on the same level. The horizontal distance between launch and landing is the range:

R=u2sin2θgR = \frac{u^2 \sin 2\theta}{g}

Setting up the problem

In projectile motion, horizontal and vertical motions are independent.

  • Horizontal: no acceleration, constant velocity ux=ucosθu_x = u\cos\theta
  • Vertical: constant downward acceleration gg, initial velocity uy=usinθu_y = u\sin\theta

Range is a horizontal quantity — it equals the horizontal velocity multiplied by the total time of flight.

R=ux×T=ucosθ×TR = u_x \times T = u\cos\theta \times T

We already know the time of flight:

T=2usinθgT = \frac{2u\sin\theta}{g}

Derivation

Substitute TT into the range equation:

R=ucosθ×2usinθgR = u\cos\theta \times \frac{2u\sin\theta}{g}

R=2u2sinθcosθgR = \frac{2u^2 \sin\theta\cos\theta}{g}

Now use the double angle identity: 2sinθcosθ=sin2θ2\sin\theta\cos\theta = \sin 2\theta

R=u2sin2θg\boxed{R = \frac{u^2\sin 2\theta}{g}}

Why the double angle identity appears

The identity sin2θ=2sinθcosθ\sin 2\theta = 2\sin\theta\cos\theta is a standard trigonometric result. It appears here naturally because the range depends on both sinθ\sin\theta (from the vertical motion, via TT) and cosθ\cos\theta (from the horizontal motion). Their product sinθcosθ\sin\theta\cos\theta is exactly half of sin2θ\sin 2\theta.

Maximum range

R=u2sin2θgR = \frac{u^2 \sin 2\theta}{g}

sin2θ\sin 2\theta is maximum when 2θ=90°2\theta = 90°, i.e. when θ=45°\theta = 45°.

At θ=45°\theta = 45°: sin90°=1\sin 90° = 1, so:

Rmax=u2gR_{\text{max}} = \frac{u^2}{g}

Key Idea
Maximum range is at $\theta = 45°$ — the angle that best balances horizontal speed and time of flight. Lower angles give more horizontal speed but less time in the air. Higher angles give more time but less horizontal speed. $45°$ is the optimal balance.

Complementary angles give the same range

If θ1+θ2=90°\theta_1 + \theta_2 = 90°, then θ2=90°θ1\theta_2 = 90° - \theta_1, and:

sin2θ2=sin(180°2θ1)=sin2θ1\sin 2\theta_2 = \sin(180° - 2\theta_1) = \sin 2\theta_1

So both angles give the same range. For example, 30°30° and 60°60° give identical ranges. So do 20°20° and 70°70°, or 15°15° and 75°75°.

θ\thetaComplementary angleRange
15°15°75°75°Same
30°30°60°60°Same
45°45°45°45°Maximum

How range varies with angle

θ\thetasin2θ\sin 2\thetaRange (as fraction of RmaxR_{\text{max}})
0°0000
15°15°0.50.50.5Rmax0.5\, R_{\text{max}}
30°30°320.87\frac{\sqrt{3}}{2} \approx 0.870.87Rmax0.87\, R_{\text{max}}
45°45°11RmaxR_{\text{max}}
60°60°320.87\frac{\sqrt{3}}{2} \approx 0.870.87Rmax0.87\, R_{\text{max}}
75°75°0.50.50.5Rmax0.5\, R_{\text{max}}
90°90°0000 — goes straight up, lands at the same spot

Assumptions

  • Launch and landing at the same height
  • No air resistance
  • gg constant throughout
Note
If the projectile is launched from a height (e.g. from a cliff), the landing point is lower than the launch point. The net vertical displacement is not zero, and the simple formula $R = \frac{u^2\sin 2\theta}{g}$ no longer applies. The time of flight must be recalculated from the actual vertical displacement.