The James Webb Space Telescope has a sun shield consisting of five layers. As a first approximation, assume that each layer is black, abosorbing all radiation that hits it, and radiating as a blackbody. Furthermore, assume the layers are large enough and close enough together that you can neglect edge effects, so that all energy radiated by one layer is absorbed by the next. Further, assume that the telescope itself is a black sphere that is much smaller in radius than the distance between it and the sun shield, which itself is much smaller than the width of the sun shield.
Once the system reaches steady state, what will the temperature of the telescope be under these assumptions?
Please start with the assumption that the visible surface of the sun is at 6000 K, and make use of the radius of the sun as well as our distance from the sun rather than simply assuming the known intensity of solar radiation. Specifically, I'd like your work to show how much the temperature drops at each stage (sun to first layer, first layer to second layer, etc).
Download the file extraterr_solar.csv, which is in comma-separated-variable (csv) format. Open the csv file in a spreadsheet program such as Excel. The data is the spectral intensity with respect to wavelength, \(S_\lambda\), for the sunlight that is hitting a satellite above the earth. The first column is wavelength in units of nanometers. The second column is spectral intensity in units of W/(m\(^2\cdot\)nm).
Consider a narrow band of wavelengths, from 552.5 nm to 557.5 nm. (The bandwidth is 5 nm and the central wavelength is 555 nm). All the photons in this bandwidth have very similar energy, \(E_{\text{photon}} \approx\) (1240 nm\(\cdot\)eV)/(555 nm). How many photons per second per \(\text{m}^2\) are in this spectral band of sunlight? Explain your method using standard mathmeatical notation. Additionally, write down the formula that you entered into the spreadsheet.
The calculation that you did for part b can now be applied to every row in your spreadsheet. You will need these numbers for part c.