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 u at angle θ. It lands back on the same level. The horizontal distance between launch and landing is the range:
R=gu2sin2θ
Setting up the problem
In projectile motion, horizontal and vertical motions are independent.
Horizontal: no acceleration, constant velocity ux=ucosθ
Range is a horizontal quantity — it equals the horizontal velocity multiplied by the total time of flight.
R=ux×T=ucosθ×T
We already know the time of flight:
T=g2usinθ
Derivation
Substitute T into the range equation:
R=ucosθ×g2usinθ
R=g2u2sinθcosθ
Now use the double angle identity: 2sinθcosθ=sin2θ
R=gu2sin2θ
Why the double angle identity appears
The identity sin2θ=2sinθcosθ is a standard trigonometric result. It appears here naturally because the range depends on both sinθ (from the vertical motion, via T) and cosθ (from the horizontal motion). Their product sinθcosθ is exactly half of sin2θ.
Maximum range
R=gu2sin2θ
sin2θ is maximum when 2θ=90°, i.e. when θ=45°.
At θ=45°: sin90°=1, so:
Rmax=gu2
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°, then θ2=90°−θ1, and:
sin2θ2=sin(180°−2θ1)=sin2θ1
So both angles give the same range. For example, 30° and 60° give identical ranges. So do 20° and 70°, or 15° and 75°.
θ
Complementary angle
Range
15°
75°
Same
30°
60°
Same
45°
45°
Maximum
How range varies with angle
θ
sin2θ
Range (as fraction of Rmax)
0°
0
0
15°
0.5
0.5Rmax
30°
23≈0.87
0.87Rmax
45°
1
Rmax
60°
23≈0.87
0.87Rmax
75°
0.5
0.5Rmax
90°
0
0 — goes straight up, lands at the same spot
Assumptions
Launch and landing at the same height
No air resistance
g 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.