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Viewing Single Post From: The giant space ship example  

Chris HoStuart  Dec 4 2011, 10:48 AM  
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At Climate Etc, gbaikie provided some comparisons and calculations to get started with the starship. I'll repeat some of them here, in tabular form. The following numbers define what is given for the ship, and can be a basis for comparison with Earth, or the moon, or other bodies.
Values for bodies in the solar system are available from NASA at the Planetary Fact Sheet. Calculating values invariably works better with SI units, so that's what I will be using. Some points to bear in mind on units: Temperature. Many thermodynamic calculations need to use an absolute temperature scale, where the coldest possible temperature is given as 0. Absolute temperature is measured in Kelvins. The temperature in degrees Celsius is equal to the temperature in Kelvin, plus 273.16; adding 273 is adequate for rough conversions. Pressure. The SI unit for pressure is the Pascal (Pa), which is the same as one Newton per square meter. The force on one kilogram in Earth's gravity is 9.8 Newtons. Earth's atmospheric pressure at sea level is very close to 100,000 Pa. The unit "hectoPascal" (hPa) is sometimes used; a hectoPascal is 100 Pascals, and this is equivalent to 1 millibar, and a "bar" is an unit representing an early estimate of pressure at Earth's surface. The "standard atmosphere" pressure is now defined to be 101325 Pa. One psi is equal to 6895 Pa. The pressure at Earth's surface in Pascals is the mass of the atmospheric column above a square meter of surface, times the gravitational acceleration. The gravitational acceleration g at the surface of a uniform sphere of mass M and radius R is equal to GM/R^{2}, where G = 6.673 e11 is the gravitational constant. Hence M = gR^{2}/G. The volume V of a sphere of radius R is (4/3).pi.R^{3}, so the density will be M/V = 0.75*g/G.R.pi. The dry adiabatic lapse rate (DALR) in an atmosphere is g/Cp (unit K/km), where Cp is the specific heat at constant pressure (in units J/g/K). For SI purists, note that these are not quite SI units; Cp is typically given as Joule per gram per Kelvin (not per kilogram), and the lapse rate in Kelvin per kilometer (not per meter). I'll use these units also, where it shows up. On Earth, where the atmosphere is mainly Nitrogen and Oxygen, Cp is very close to 1. On Mars, the atmosphere is mainly Carbon Dioxide, with Cp being about 0.83, so there the DALR is about 3.71/0.83, or the DALR is thus about 9.8. For an atmosphere consisting mainly of Nitrogen and Oxygen, the specific heat (at constant pressure) Cp is pretty close to 1 (unit J/g/K); and the DALR is about 4.5. In the starship, Cp should be similar to Earth, since you want an atmosphere that is mostly Nitrogen and Oxygen, both of which have Cp close to 1. Hence the DALR will be about 1 as well. Using these formulae, we can find some basic properties for Earth, Mars, our Moon, and the starship.
(late edit to fix the DALR on Mars; I previously had 3.7 which failed to account for the reduced Cp value.) Gbaikie, this matches your estimates so far, apart from lapse rate. You were correct to suppose a weaker lapse rate on the starship than on Earth or Mars; but it's weaker even than you had guessed. Edited by Chris HoStuart, Dec 4 2011, 09:59 PM.
 
The giant space ship example · Physical theory for climate 