The visible spectrum of wavelengths is about \(400\text{ nm}-700\text{ nm}\). The middle of this range is 550 nm, so I'll simplify my analysis by assuming all the photons have wavelength 550 nm. The energy of each photon is \begin{align} E_{a}&=\frac{hc}{\lambda_a}\\ &=\frac{(3\times10^8)(6.6\times10^{-34})}{(550\times10^{-9})}\text{ J}\\ &= \frac{2\times10^{-25}}{5.5\times10^{-7}}\text{ J}\\ &=3.6\times10^{-19}\text{ J}\\ \notag\\ \end{align}
the corresponding rates of photon emission from the 20 watt lightbulb \begin{align} R_{a}&=\frac{P}{E_{a}}\\ &=\frac{20}{3.6\times10^{-19}}\text{ s}^{-1}\\ &=5.6\times10^{19}\text{ s}^{-1}\\ \notag \\ \end{align}
The surface area of the sphere with radius \(100\text{ m}\) is \begin{align} S_1 = 4\pi 100^2 \text{ m}^2=130000\text{ m}^2 \end{align} and the area of the pupil is \begin{equation} S_2 = \pi \left(\frac{8}{2}\right)^2 \text{mm}^2=50 \text{ mm}^2 = 5\times10^{-7}\text{ m}^2 \end{equation} So the portion of the light from the bulb that enters the eye is approximately \begin{equation} \frac{S_2}{S_1} = \frac{5\times10^{-7}}{1.3\times10^5} =4\times10^{-12} \end{equation} So the number of photons that enters the eye is approximately, \begin{align} (4\times10^{-12})\times (5.6 \times 10^{19}) = 1.6\times10^8\text{ s}^{-1} \end{align}
This is easily visible to the human eye (the human eye could see a point source emitting \(1.5 \times 10^4\) photons per second).
Calculate \(E_4\) and \(E_5\) \begin{align} E_4 = \frac{-13.6\text{ eV}}{4^2} = -0.85\text{ eV}\\ E_5 = \frac{-13.6\text{ eV}}{5^2} = -0.544\text{ eV}\\ \Delta E = 0.306 eV\\ \end{align} To find the wavelength in nanometers, I'll use the \(hc=1240\text{ eV.nm}\): \begin{align} \lambda = \frac{1240\text{ eV.nm}}{0.306\text{ eV}} = 4050\text{ nm} \end{align}
\begin{align} &E_1 = \hbar \omega \left(\frac{3}{2}\right)\\ &E_0 = \hbar \omega \left(\frac{1}{2}\right)\\ &\Delta E = \hbar \omega = (1.05\times10^{-34})(10^{16})\text{ J}\\ & \quad \quad \quad \quad = 1.05\times 10^{-18} \text{ J} \\ & \quad \quad \quad \quad = 6.6 \text{ eV} \\ & \lambda = \frac{h c}{E_{photon}} = \frac{h c}{\hbar \omega} = \frac{1240 \text{ nm eV}}{6.6 \text{ eV}} = 190 \text{ nm} \end{align} If we applied a classical analysis (no quantum mechanics), we would expect light with frequency \(\omega/2\pi\). \begin{align} \lambda = \frac{c}{f} = \frac{hc}{hf} = \frac{hc}{\hbar \omega} = 190\text{ nm} \end{align} Exactly the same result.
Suppose an electron is trapped in a box whose length is \(L= 1.2 \text{ nm}\). This is a coarse-grained model for an electron in a small molecule like cyanine (see Example Q11.1 in the textbook, and the figure above). If we solve the Schrodinger equation for this coarse-grained model, the possible energy levels for this electron are \begin{align} E = \frac{h^2 n^2}{8 m L^2} \end{align} where \(m\) is the mass of the electron and \(n= 1,\ 2,\ 3,\ ...\)
Draw a spectrum chart (like the righthand side of Figure Q11.2) to show what you would see if a number of identical excited systems of this type emitted light that was dispersed by a diffraction grating.
Note: Due to the shape/symmetries of electron wavefunctions in a box, optical transitions between energy levels only happen when \(\Delta n = n_\text{initial}-n_\text{final}\), is an odd integer.
Visible photons
The energy levels fro the electron are \begin{align} E_n &= \frac{h^2 n^2}{8 m L^2} \qquad \qquad \text{ where } L = 1.12\text{ nm}\\ &= \left[\frac{(6.6\times10^{-34})^2}{8 (9\times10^{-31}) (1.2\times10^{-9})^2}\right] n^2\\ &\approx [0.4\times10^{-19}\text{ J}]n^2\\ &=[0.25\text{ eV}]n^2 \end{align} First I'll look at transitions with \(\Delta n = 1\), for example \(n=4\) to \(n=3\).
Now I'll check transitions with \(\Delta n=3\), for example \(n=4\) to \(n=1\).
If \(\Delta n=5\) the system would emit photons of 3.75 eV or greater (outside the visible spectrum).![]()
In conclusion, there are four energies of visible photons that this system could emit: 2 eV, 2.25 eV, 2.75 eV and 3 eV.
The first spacecraft using a solar sail for propulsion was launched in 2010. Its name is IKAROS. It has a square sail with dimensions 14 m x 14 m. Assume that the sail's mass is 2 kg and it reflects 100% of incident photons. When IKAROS is loaded with other equipment, the total mass of the vehicle is 10 kg. The sail is orientated to receive maximum light from the sun.
First, find the energy hitting the solar sail in one second \begin{align} \text{Energy}=1300 \text{ J/(m$^2$.s)} \times 1 \text{ s} \times200 \text{ m}^2 = 2.6 \times 10^{5} \end{align} \begin{align} \text{Momentum}=\frac{E}{c}=\frac{2.6 \times 10^{5} \text{ J}}{3 \times 10^8 \text{ m/s}} \approx 10^{-3} \text{ kg.m/s} \end{align}
The photons are reflected (reverse their direction), so the solar sail must receive twice the incoming momentum (for conservation of momentum to be satisfied). So, I mulltiply by 2. There are 86000 seconds in a day, so I also multiply by 86000. \begin{align} \text{Momentum transfer per day} = 8.6 \times 10^4 \times 2 \times 10^{-3} \text{ kg.m/s} \approx 150 \text{ kg.m/s} \end{align}
The spacecraft has a mass of 10 kg, so the change in velocity in one day must be 15 m/s.