| Quantity | Expression | Notes |
|---|---|---|
| Gravitational field (radial) | \(\displaystyle \mathbf g(r)= -\frac{GM}{r^{2}}\hat{\mathbf r}\) | Vector; points toward the mass. |
| Gravitational potential | \(\displaystyle \phi(r)= -\frac{GM}{r}\) | Scalar; zero conventionally at ∞. |
| Potential energy of a test mass m | \(\displaystyle U = m\phi = -\frac{GMm}{r}\) | Negative because work must be done against gravity to reach ∞. |
| Relation between field and potential | \(\displaystyle \mathbf g = -\nabla\phi\) | For a radial field, \(\mathbf g = -\frac{d\phi}{dr}\hat{\mathbf r}\). |
| Escape velocity from a body of mass M and radius R | \(\displaystyle v_{\text{esc}} = \sqrt{\frac{2GM}{R}}\) | Derived from \(\tfrac12mv_{\text{esc}}^{2}=GMm/R\). |
| Orbital speed in a circular orbit of radius r | \(\displaystyle v_{\text{orb}} = \sqrt{\frac{GM}{r}}\) | Set centripetal acceleration \(v^{2}/r\) equal to \(|\mathbf g|\). |
| Total mechanical energy of a circular orbit | \(\displaystyle E_{\text{tot}} = U + K = -\frac{GMm}{2r}\) | Kinetic energy \(K = +\frac{GMm}{2r}\). |
\(\displaystyle \mathbf g(r)= -\frac{GM}{r^{2}}\hat{\mathbf r}\).
\(\displaystyle g_{\oplus}\approx 9.81\ \text{m s}^{-2}\).
Definition: The gravitational potential φ at a point is the work done per unit mass in bringing a small test mass from infinity to that point (the zero of potential is chosen at ∞).
\(dW = -F\,dr = -\dfrac{GMm}{r^{2}}\,dr\).
\[
W = -\int_{\infty}^{r}\frac{GMm}{r^{2}}\,dr
= -GMm\Bigl[-\frac{1}{r}\Bigr]_{\infty}^{r}
= -\frac{GMm}{r}.
\]
\[
\phi(r)=\frac{W}{m}= -\frac{GM}{r}.
\]
\[
U = -\int_{\infty}^{r}\mathbf g\cdot d\mathbf r.
\]
To escape to infinity the kinetic energy must equal the magnitude of the gravitational potential energy at the surface:
\[
\frac12 mv_{\text{esc}}^{2}= \frac{GMm}{R}\;\Longrightarrow\;
v_{\text{esc}}=\sqrt{\frac{2GM}{R}}.
\]
For a satellite in a circular orbit of radius r, the required centripetal acceleration is provided by the gravitational field:
\[
\frac{v_{\text{orb}}^{2}}{r}= \frac{GM}{r^{2}}
\;\Longrightarrow\;
v_{\text{orb}}=\sqrt{\frac{GM}{r}}.
\]
Kinetic energy \(K = \tfrac12 mv_{\text{orb}}^{2}= \dfrac{GMm}{2r}\).
Total mechanical energy:
\[
E_{\text{tot}} = K + U = \frac{GMm}{2r} - \frac{GMm}{r}= -\frac{GMm}{2r}.
\]
The negative sign shows the orbit is a bound state.
\(\phi' = -\dfrac{GM}{r}+ \dfrac{GM}{R_{\oplus}}\), which is zero at the surface and positive above it.
A simple classroom experiment:
\(\displaystyle g = \frac{4\pi^{2}L}{T^{2}}\).
\[
\Delta\phi = -\int{h{1}}^{h{2}} g\,dh \approx -g\,(h{2}-h_{1}).
\]
This satisfies the A‑Level requirement for experimental skills (AO3) and links the measured field to the concept of potential.
| Symbol | Quantity | Unit |
|---|---|---|
| \(G\) | Universal gravitational constant | \(6.674\times10^{-11}\ \text{N m}^{2}\text{kg}^{-2}\) |
| \(M\) | Mass producing the field | kg |
| \(m\) | Test mass (or satellite) | kg |
| \(r\) | Distance from the centre of M | m |
| \(\mathbf g\) | Gravitational field strength | m s⁻² |
| \(\phi\) | Gravitational potential | J kg⁻¹ |
| \(U\) | Gravitational potential energy | J |
| \(v_{\text{esc}}\) | Escape velocity | m s⁻¹ |
| \(v_{\text{orb}}\) | Orbital speed (circular) | m s⁻¹ |
Given:
Potential (zero at ∞):
\[
\phi{\oplus}= -\frac{GM{\oplus}}{R_{\oplus}}
\approx -\frac{6.674\times10^{-11}\times5.97\times10^{24}}{6.37\times10^{6}}
\approx -6.3\times10^{7}\ \text{J kg}^{-1}.
\]
Potential energy of a 1 kg mass at the surface:
\[
U = m\phi_{\oplus} \approx -6.3\times10^{7}\ \text{J}.
\]
Escape velocity from the Earth:
\[
v{\text{esc}} = \sqrt{\frac{2GM{\oplus}}{R_{\oplus}}}
\approx 11.2\ \text{km s}^{-1}.
\]
The gravitational field g describes the force per unit mass, while the gravitational potential φ describes the work per unit mass required to bring a test mass from infinity to a point. For a point mass M:
These quantities are linked by \(\mathbf g = -\nabla\phi\). Choosing a convenient reference point for potential does not affect physical results, only the numerical value of φ. The concepts are applied to escape velocity, orbital motion, and energy calculations—core topics for Cambridge AS & A‑Level Physics.
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