Throw a stone straight up and it falls back. Throw it harder and it rises higher before it falls. In November 2013 India's Mars Orbiter Mission, Mangalyaan, left its orbit round the Earth for Mars. It never came back. Somewhere between a stone and Mangalyaan lies a speed beyond which the Earth can no longer call a body home.
Energy decides escape
Launch a body of mass \(m\) from the surface of a planet of mass \(M\) and radius \(R\), with speed \(v\). Ignore the air. After launch only gravity acts, and gravity is conservative. So the total energy \(E = K + U\) stays constant along the whole flight.
At the surface \(E = \tfrac12 mv^2 - GMm/R\). Far away \(U\) approaches zero, so there \(E\) is all kinetic energy, which cannot be negative. So the body can reach infinity only if \(E \ge 0\). The least launch speed that does it makes \(E = 0\) exactly: the body arrives at infinity with no speed to spare. This least speed is the escape speed \(v_e\), usually called the escape velocity.
The escape speed from a planet is the least speed with which a body must leave its surface to reach infinity and never return. Air resistance is ignored. It makes the total energy of the body and the planet exactly zero.
\[ \tfrac12 mv_e^2 - \dfrac{GMm}{R} = 0 \]
Why. at the least escape speed the total energy is exactly zero.
?
Your turn. move the potential term across and divide by \(m/2\). Which line is it?
\[ v_e = \sqrt{\dfrac{2GM}{R}} = \sqrt{2gR} \]
Read it. take the square root, and put \(GM = gR^2\).
For the Earth, \(v_e = \sqrt{2 \times 9.8 \times 6.4 \times 10^6} = 1.12 \times 10^4\,\text{m/s}\), that is \(11.2\,\text{km/s}\). That is about \(40\,000\,\text{km/h}\), some forty times the speed of a passenger jet. For the Moon, with a mass of \(7.35 \times 10^{22}\,\text{kg}\) and a radius of \(1.74 \times 10^6\,\text{m}\), the same formula gives only \(2.4\,\text{km/s}\).
A planet has the same density as the Earth but twice its radius. Find its escape speed in km/s, taking the Earth's as \(11.2\,\text{km/s}\).
The well, drawn
In the chapter on Potential Energy and Conservation of Energy you read energy diagrams. A curve shows \(U\), a level line shows \(E\), and the gap between them is \(K\). Draw one for a body and the Earth. The curve \(U = -GMm/r\) starts at \(-GMm/R\) at the surface and rises towards zero far away, but never reaches it. It is a well with a sloping wall and no rim, the gravitational well.
Set \(E = -0.5\,GMm/R\) and press play. The body leaves the surface with the gap \(K\) between the line and the curve. As it rises, the gap closes. At \(r = 2R\) the line meets the curve, so \(K = 0\), and the body starts to fall. A negative total energy always meets the curve somewhere, at \(r = GMm/|E|\). So the body is bound: it can never go beyond that distance.
Now raise \(E\) to zero or above. The curve approaches zero only from below, so the line never meets it. The gap \(K\) never closes, and the body climbs out for ever. It is unbound. The dividing line is \(E = 0\), and on the Earth that needs exactly \(11.2\,\text{km/s}\) at launch.
The zero at infinity is what makes "escaped" mean something. With that choice, every bound body has a negative total energy and every free body a positive one. Another zero would not change the physics. But the sign would no longer tell you at a glance whether a body can leave.
For a body launched straight up with \(v < v_e\), energy gives the greatest height \(h\) at once. Put \(\tfrac12 mv^2 - GMm/R = -GMm/(R + h)\) and use \(v_e^2 = 2GM/R\). The result is \(h = Rv^2/(v_e^2 - v^2)\). At \(v = 7.9\,\text{km/s}\), where \(v^2 = v_e^2/2\), the body rises to \(h = R\), a height of \(6400\,\text{km}\).
A probe is launched straight up from the Earth at \(5.6\,\text{km/s}\). Ignore the air. Take \(v_e = 11.2\,\text{km/s}\) and \(R = 6400\,\text{km}\). How high does it rise above the surface, in km?
A probe leaves the Earth with a total energy \(E = -2 \times 10^9\,\text{J}\), taking \(U = 0\) at infinity. What happens to it?
Mass and direction do not matter
In the derivation, the mass \(m\) of the body cancelled. Both its kinetic energy and its potential energy are proportional to \(m\). So a pebble and a loaded rocket need the same \(11.2\,\text{km/s}\). The rocket needs far more energy, of course, but the same speed.
Energy is a scalar, so the direction of launch never entered either. A body thrown upward, sideways or at a slant with the same speed has the same total energy. As long as its path does not strike the ground, it escapes. The paths differ in shape, but every one of them climbs away for ever.
A launch faster than \(v_e\) leaves some kinetic energy over at infinity. There \(U = 0\), so \(\tfrac12 mv_\infty^2 = \tfrac12 mv^2 - \tfrac12 mv_e^2\). This gives \(v_\infty = \sqrt{v^2 - v_e^2}\). A launch at \(15\,\text{km/s}\) keeps only \(\sqrt{225 - 125} = 10\,\text{km/s}\) far from the Earth. The speed on the way out is lost much faster than a simple subtraction of \(11.2\) suggests.
"Escape velocity" is really a speed. It has no direction, because the energy that decides escape has none. Also, it is the speed at the surface for a coasting body. A rocket that fires its engine all the way up never needs to reach \(11.2\,\text{km/s}\) near the ground.
A probe is launched from the Earth at \(15\,\text{km/s}\) and coasts away. Ignore the air and the Sun. What is its speed far from the Earth, in km/s? Take \(v_e = 11.2\,\text{km/s}\).
Which statements about the escape speed from the Earth's surface are true? Ignore the air.
Why the Moon has no air
The molecules of a gas move in all directions at many speeds. Oxygen molecules at \(120\,°\text{C}\), the temperature of the Moon's surface at noon, have a typical speed of about \(0.55\,\text{km/s}\). A very small fraction of them move three or four times faster than that. The escape speed does not depend on what is moving. So a molecule at the top of an atmosphere that exceeds \(v_e\) and heads upward is lost for ever.
The fast molecules that leave are replaced, as collisions give a new few a high speed. So an atmosphere leaks slowly, and the leak is fast when \(v_e\) is only a few times the typical molecular speed. A useful rule of thumb follows. A planet keeps a gas for billions of years only if its \(v_e\) exceeds about six times the gas's typical speed.
Use the rule of six. The typical speed of an oxygen molecule is about \(0.55\,\text{km/s}\) at the Moon's noon temperature. Can the Moon keep oxygen? Can the Earth, with \(v_e = 11.2\,\text{km/s}\)?
(a) Six times \(0.55\,\text{km/s}\) is \(3.3\,\text{km/s}\). The Moon's escape speed, \(2.4\,\text{km/s}\), falls short. Over billions of years the Moon loses its oxygen, and lighter gases leave even sooner.
(b) The Earth's escape speed, \(11.2\,\text{km/s}\), is more than three times \(3.3\,\text{km/s}\). The Earth holds its oxygen and nitrogen with a wide margin.
(c) The lightest gas, hydrogen, is another story. High in the Earth's air, near \(1000\,\text{K}\), its typical speed is about \(3.5\,\text{km/s}\), and six times that exceeds \(11.2\,\text{km/s}\). That is why the Earth's air holds almost no free hydrogen.
Why has the Moon lost the atmosphere it may once have had, while the Earth kept its air?
From Sriharikota, ISRO launches most rockets towards the east. The ground there already moves eastward at about \(0.45\,\text{km/s}\) because the Earth spins. A rocket fired east starts with that speed for free. The escape speed from the Earth's surface is the same in every direction. What the spin changes is how much of that speed the rocket itself must supply.
The hook asked for the speed at which a thrown body never returns. From the Earth's surface it is \(11.2\,\text{km/s}\), whatever the body and whatever the direction. The Moon, with \(v_e = 2.4\,\text{km/s}\), cannot hold even the slow-moving molecules of oxygen for long, and so its sky is black by day.
- Thinking that a heavier body needs a greater escape speed.The mass cancels. The escape speed depends only on the planet, \(\sqrt{2GM/R}\).
- Subtracting speeds to find the speed far away.Subtract squares: \(v_\infty = \sqrt{v^2 - v_e^2}\).
- Using \(h = v^2/2g\) for a launch of several km/s.The pull weakens with height. Use energy with \(U = -GMm/r\): \(h = Rv^2/(v_e^2 - v^2)\).