Physics · Gravitation

Variation of g with Altitude & Depth

The value $g = 9.8~\text{m s}^{-2}$ holds only at the Earth's surface. Climb a mountain and it falls; sink down a mine shaft and it falls again — but for two different reasons, with two different formulas. NCERT §7.6 derives both: above the surface $g$ drops as the inverse square of distance from the centre, while below the surface it drops linearly to zero at the centre. Rotation and the Earth's slightly flattened shape add a third variation with latitude. This deep-dive builds the three formulas, contrasts the height-versus-depth fall-off on a single graph, and works the NEET-favourite tunnelling and "equal g" problems.

The surface value as baseline

The acceleration due to gravity at the Earth's surface follows from Newton's law of gravitation applied to a body of mass $m$ resting on a sphere of mass $M_E$ and radius $R$:

$$g = \frac{G M_E}{R^2} \approx 9.8~\text{m s}^{-2}.$$

This single number is the reference against which every variation is measured. Two facts drive everything below. First, $g$ depends on the distance from the centre of the Earth — so moving away weakens gravity. Second, the surface value uses the entire mass $M_E$, true only while all the Earth's mass stays below you; burrow inside and part of the mass ends up above you and stops pulling you down. These two ideas — distance and enclosed mass — split the problem cleanly into the height case and the depth case. For the surface derivation in full, see acceleration due to gravity.

Variation with height above the surface

Take a body at a height (altitude) $h$ above the surface. Its distance from the centre is now $R + h$, and the whole mass $M_E$ still lies below it. Newton's law gives the exact value:

$$g_h = \frac{G M_E}{(R+h)^2} = g\,\frac{R^2}{(R+h)^2} = \frac{g}{\left(1 + \dfrac{h}{R}\right)^2}.$$

This is the form to use whenever $h$ is comparable to $R$ — satellites, distant orbits, "height equal to half the radius" type problems. NIOS §5.3.1 notes the immediate consequence: at $h = R$, the distance from the centre doubles to $2R$, so $g$ falls to one-quarter of its surface value.

When the altitude is small compared with the radius ($h \ll R$) — aircraft, mountains, towers — the binomial expansion of $(1 + h/R)^{-2}$ keeping only the first-order term gives the working approximation NCERT §7.6 quotes:

$$g_h \approx g\left(1 - \frac{2h}{R}\right), \qquad h \ll R.$$

The factor of 2 is the signature of the inverse-square law: a fractional rise $h/R$ in distance produces twice that fractional drop in $g$. NIOS Example 5.2 illustrates the scale — at a typical cruising altitude of 10 km, with $R = 6400$ km, the value of $g$ falls only to about $9.77~\text{m s}^{-2}$, a change of roughly 0.3%.

Variation with depth below the surface

Now drop a body to a depth $d$ below the surface, so its distance from the centre is $r = R - d$. Two things change at once. The distance shrinks, which on its own would increase $g$. But the spherical shell of matter above the body — the outer shell of thickness $d$ — now contributes nothing: NIOS §5.3.2 states the standard shell result that the net gravitational force from a uniform spherical shell on a point inside it is exactly zero. Only the inner sphere of radius $r = R - d$ pulls the body.

Assuming the Earth has uniform density $\rho$, the mass of that inner sphere is $M' = \tfrac{4}{3}\pi\rho\,(R-d)^3$, and the acceleration at depth $d$ becomes

$$g_d = \frac{G M'}{(R-d)^2} = \frac{4}{3}\pi G \rho\,(R-d).$$

Since the surface value is $g = \tfrac{4}{3}\pi G \rho R$ (set $d = 0$), dividing one by the other removes the constants and leaves the clean linear law NCERT §7.6 gives:

$$g_d = g\left(1 - \frac{d}{R}\right), \qquad 0 \le d \le R.$$

The fall-off is linear in $d$ and the coefficient is just $d/R$ — no factor of 2. The single most important consequence: set $d = R$ (the body has reached the centre) and $g_d = 0$. At the centre of the Earth, matter surrounds you symmetrically in every direction and the pulls cancel exactly.

The g-versus-distance graph

The two laws meet at the surface and behave oppositely on either side of it. Plotting $g$ against distance $r$ from the centre makes the whole story visible in one curve: a straight line rising from zero at the centre to the peak at $r = R$, then an inverse-square tail decaying beyond the surface.

distance from centre, r g R (surface) g O 2R g/4 g_d = g(1 − d/R) · linear g_h = gR²/(R+h)² · inverse-square g max at surface INSIDE (depth) OUTSIDE (height)
Variation of $g$ with distance $r$ from the centre of the Earth (uniform-density model). Below the surface ($r < R$) the curve is the straight line $g_d = g(1 - d/R)$, rising from $g = 0$ at the centre. Above the surface ($r > R$) it is the inverse-square tail $g_h = gR^2/(R+h)^2$. The two meet at the peak $r = R$, where $g$ is maximum — at $r = 2R$ it has fallen to $g/4$. Adapted from NIOS Fig. 5.5.

Read the graph from the centre outwards. At $r = 0$, $g = 0$. The line climbs steadily to its maximum at the surface. Beyond the surface, $g$ never increases again — the inverse-square tail only decays, passing through $g/4$ at $r = 2R$. The surface is the unique peak of the entire curve.

Height vs depth — the contrast

Place the three variations side by side. They share a starting point — the surface value $g$ — but differ in mechanism, in the fall-off coefficient, and in how fast they decay.

Height

Above the surface

$g_h = \dfrac{gR^2}{(R+h)^2}$ $\approx g\!\left(1 - \dfrac{2h}{R}\right)$, $h\ll R$

Mechanism: full mass below, distance grows. Inverse-square decay, never reaches zero.

Depth

Below the surface

$g_d = g\!\left(1 - \dfrac{d}{R}\right)$ $= \dfrac{4}{3}\pi G\rho\,(R-d)$

Mechanism: overlying shell cancels, enclosed mass shrinks. Linear decay to exactly zero at the centre.

Latitude

Along the surface

$g' = g - \omega^2 R\cos^2\!\lambda$ max at poles, min at equator

Mechanism: rotation diverts part of gravity to centripetal force; flattened shape adds a smaller radius at the poles.

The decisive comparison: for the same small displacement $x$ from the surface, going up changes $g$ by $-2gx/R$ while going down changes it by only $-gx/R$. Height kills $g$ twice as fast as depth. That is the engine behind the NEET-favourite question "at what depth is $g$ the same as at height $h$" — the answer is $d = 2h$, because depth must travel twice as far to lose the same amount.

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Related drill

This whole topic rests on the surface formula $g = GM_E/R^2$ — revisit its derivation and the mass-of-the-Earth estimate in acceleration due to gravity.

Variation with latitude and shape

Even staying exactly on the surface, $g$ is not the same everywhere — it depends on latitude $\lambda$ (the angular distance north or south of the equator). NIOS §5.3.3 traces this to the Earth's daily rotation. Every point on the surface moves in a circle about the rotation axis, and circular motion needs centripetal force. Part of the gravitational pull is "spent" supplying that force, so the effective gravity an object actually experiences is reduced:

$$g' = g - \omega^2 R\cos^2\!\lambda,$$

where $\omega$ is the Earth's angular speed of rotation. The radius of a point's circular path is $R\cos\lambda$, and only the component of the centripetal term along the local vertical reduces $g$, which together produce the $\cos^2\lambda$ dependence.

  • At the equator ($\lambda = 0$, $\cos^2\lambda = 1$): the reduction is largest, $g' = g - \omega^2 R$. This is the smallest effective $g$ on Earth.
  • At the poles ($\lambda = 90^\circ$, $\cos^2\lambda = 0$): the rotation term vanishes, $g' = g$. The poles lie on the rotation axis, trace no circle, and need no centripetal force — so the effective $g$ is largest there.

NIOS confirms the magnitude is small: with $\omega = 7.27\times10^{-5}~\text{rad s}^{-1}$ and $R \approx 6.37\times10^6$ m, the maximum correction $\omega^2 R$ is only about $0.034~\text{m s}^{-2}$ — a fraction of a percent of $g$.

A second, independent effect reinforces the same trend. The Earth is not a perfect sphere; rotation has flattened it so the equatorial radius is larger than the polar radius. Because $g \propto 1/R^2$, the smaller polar radius gives a larger $g$ at the poles. Both the rotation effect and the shape effect therefore point the same way: $g$ is maximum at the poles and minimum at the equator.

Worked examples

NCERT Example 7.16

Assuming the Earth to be a sphere of uniform mass density, how much would a body weigh half way down to the centre of the Earth if it weighed 250 N on the surface?

Set up. "Half way down to the centre" means depth $d = R/2$. Use the depth law $g_d = g(1 - d/R)$, and remember weight is proportional to $g$ since $W = mg$.

Compute the factor. $\dfrac{g_d}{g} = 1 - \dfrac{d}{R} = 1 - \dfrac{R/2}{R} = 1 - \dfrac{1}{2} = \dfrac{1}{2}.$

Scale the weight. $W_d = W\left(1 - \dfrac{d}{R}\right) = 250 \times \dfrac{1}{2} = \boxed{125~\text{N}}.$ The body weighs half as much half way to the centre — and would weigh nothing at the centre itself.

Worked Example — g at altitude

Compute the value of $g$ at an altitude of 10 km. Take $R = 6400$ km and the surface value $g = 9.8~\text{m s}^{-2}$.

Choose the formula. Here $h = 10$ km $\ll R = 6400$ km, so the small-height approximation $g_h = g(1 - 2h/R)$ is valid.

Substitute. $\dfrac{2h}{R} = \dfrac{2 \times 10}{6400} = 3.125\times10^{-3}.$ Then $g_h = 9.8\,(1 - 0.003125) = 9.8 \times 0.99688 \approx 9.77~\text{m s}^{-2}.$

Read it. Even at a typical aircraft cruising altitude, $g$ falls by only about 0.3%. (NIOS Example 5.2.) This is why aircraft and tower problems can safely use the linear approximation — the height is tiny next to $R$.

Worked Example — exact form at large height

A body weighs 72 N on the surface of the Earth. What is the gravitational force on it at a height equal to half the radius of the Earth? (NEET 2020)

Spot the trap. Here $h = R/2$ is not small compared with $R$, so the $g(1-2h/R)$ approximation fails. Use the exact $g_h = g\,R^2/(R+h)^2$.

Compute the factor. $\dfrac{g_h}{g} = \dfrac{R^2}{(R + R/2)^2} = \dfrac{R^2}{(3R/2)^2} = \dfrac{1}{9/4} = \dfrac{4}{9}.$

Scale the weight. $W_h = 72 \times \dfrac{4}{9} = \boxed{32~\text{N}}.$ The linear approximation would have wrongly given $72(1 - 1) = 0$ N — a textbook demonstration of why the exact form is mandatory when $h \sim R$.

Quick recap

Variation of g in one breath

  • Surface: $g = GM_E/R^2 \approx 9.8~\text{m s}^{-2}$ — the baseline and the maximum.
  • Height (exact): $g_h = gR^2/(R+h)^2$. Small height: $g_h \approx g(1 - 2h/R)$. Inverse-square; note the factor 2.
  • Depth: $g_d = g(1 - d/R)$, linear, valid for uniform density. $g = 0$ at the centre ($d = R$). No factor 2.
  • Latitude: $g' = g - \omega^2 R\cos^2\lambda$. Maximum at the poles, minimum at the equator; the flattened shape adds the same trend.
  • Contrast: height lowers $g$ twice as fast as depth, so "equal $g$" gives $d = 2h$.
  • Graph: straight line up to the surface, inverse-square tail beyond it; peak at $r = R$, $g/4$ at $r = 2R$.

NEET PYQ Snapshot — Variation of g

Height, depth and the "equal-g" comparison are repeat NEET themes. Same toolkit each time: pick the exact or approximate form, then scale weight as $W \propto g$.

NEET 2017

The acceleration due to gravity at a height 1 km above the Earth is the same as at a depth $d$ below the surface of the Earth. Then:

  1. $d = 2$ km
  2. $d = \tfrac{3}{2}$ km
  3. $d = 1$ km
  4. $d = \tfrac{1}{2}$ km
Answer: (1) d = 2 km

Equate the two laws. $g_h = g_d \Rightarrow g\!\left(1 - \tfrac{2h}{R}\right) = g\!\left(1 - \tfrac{d}{R}\right)$. The $g$ and $R$ cancel, leaving $2h = d$, so $d = 2 \times 1 = 2$ km. The factor of 2 from the height side is the whole point.

NEET 2020

A body weighs 72 N on the surface of the Earth. What is the gravitational force on it, at a height equal to half the radius of the Earth?

  1. 32 N
  2. 30 N
  3. 24 N
  4. 48 N
Answer: (1) 32 N

Exact inverse-square (h = R/2 is large). $W_h = \dfrac{W}{(1 + h/R)^2} = \dfrac{72}{(1 + 1/2)^2} = \dfrac{72}{9/4} = 32$ N. Using the $1-2h/R$ approximation here is the planted error.

NEET 2016

At what height from the surface of the Earth are the gravitational potential and the value of $g$ equal to $-5.4\times10^7~\text{J kg}^{-1}$ and $6.0~\text{m s}^{-2}$ respectively? Take the radius of the Earth as 6400 km.

  1. 1600 km
  2. 1400 km
  3. 2000 km
  4. 2600 km
Answer: (4) 2600 km

Use the ratio at height. $V_h = -\dfrac{GM}{R+h}$ and $g_h = \dfrac{GM}{(R+h)^2}$, so $\dfrac{|V_h|}{g_h} = R + h = \dfrac{5.4\times10^7}{6.0} = 9.0\times10^6$ m $= 9000$ km. Hence $h = 9000 - 6400 = 2600$ km — a direct application of the exact height form alongside potential.

FAQs — Variation of g with Altitude & Depth

The height-versus-depth confusions NEET aspirants get wrong most often.

Why is the height correction 2h/R but the depth correction only d/R?
They come from two different physical effects. Going up, the whole mass of the Earth stays below you but you move farther from its centre, so $g$ falls as the inverse square of distance; expanding $(1+h/R)^{-2}$ for small $h$ gives the factor $(1-2h/R)$ — note the 2. Going down, the distance to the centre shrinks (which would raise $g$), but the shell of matter above you no longer pulls you inward and the effective attracting mass falls with $(R-d)$; the combined result is the linear factor $(1-d/R)$ — no 2.
Is the formula g_h = g(1 − 2h/R) exact?
No. It is the first-order approximation valid only when $h \ll R$. The exact expression is $g_h = gR^2/(R+h)^2$. For aircraft and most tall structures (h up to a few tens of km) the approximation is accurate to better than a percent, but for heights of order $R$ — satellites, "half the radius" problems — you must use the exact inverse-square form.
What is the value of g at the centre of the Earth?
Zero. Putting $d = R$ in $g_d = g(1 - d/R)$ gives $g_d = 0$. Physically, at the centre the entire mass of the Earth is distributed symmetrically around you in all directions, so the gravitational pulls cancel and there is no net acceleration.
Where is g maximum — at the surface, above it, or below it?
For a uniform-density Earth, $g$ is maximum at the surface. Move up and it falls as the inverse square of distance; move down and it falls linearly to zero at the centre. The surface is therefore the peak of the $g$-versus-distance curve.
Why is g greater at the poles than at the equator?
Two reasons. First, the Earth's rotation: part of gravity supplies the centripetal force needed to keep you moving in a circle, and the effective value becomes $g' = g - \omega^2 R\cos^2\lambda$, largest at the poles ($\lambda = 90^\circ$, $\cos\lambda = 0$) and smallest at the equator ($\lambda = 0$). Second, the Earth is slightly flattened, so the polar radius is smaller than the equatorial radius, and a smaller radius means a larger $g$. Both effects make $g$ a maximum at the poles.
At what depth does g equal its value at a given height?
Equate $g(1 - 2h/R) = g(1 - d/R)$. The $g$ and $R$ cancel to give $d = 2h$. So the depth that reproduces a given height's $g$ is exactly twice that height. This is a recurring NEET question (asked in 2017) — the answer is always $d = 2h$, not $d = h$.
Does the depth formula assume the Earth has uniform density?
Yes. The clean linear result $g_d = g(1 - d/R)$ follows from treating the Earth as a sphere of uniform mass density. The real Earth has a dense core, so $g$ actually rises slightly before falling as you descend. NEET problems explicitly state "assuming uniform density", which licenses the linear formula.