This should be fine as a first approximation if this is in interstellar space, although the geometry of the ship would make some radiative directions preferred compared to others. This is, of course, especially true if there is a star nearby.Destructionator XIII wrote:Trying to figure it out myself, I figure if I take the temperature of one spaceship, plug it into the Stefan-Boltzmann law to get the power radiated, than from there apply an inverse square formula at the distance separating the two ships, I should have the amount of power per square meter (called the power flux, right?) hitting the telescope. Then I can get an energy number from the surface area of the telescope and the duration of the exposure.
Well, yes, but if the telescope is only responsive in some limited range of the electromagnetic spectrum, as would be more realistic, then one should integrate the Planck law over that range instead.Destructionator XIII wrote:If that energy number is large enough, it should be visible.
If the ship is far away from stars, certainly. Inside a star system, one would need to consider reflection along with the thermal radiation.Destructionator XIII wrote:1) Is my reasoning above correct? If not, what is the right way to do it? Does this also work for the temperature of the rocket fuel being expended?
Well, that's a bit complicated. Assuming the only radiation source is thermal, take the Planck law, multiply it by the luminosity function exp[-(λ-560.3)²/60.64²], where λ is the wavelength in nm, and integrate over the entire spectrum. The result is the luminous flux in watts; the measure in lumens is 683 times this amount (the same measure one gets on the light bulb packages). This particular model comes from fitting a Gaussian curve on the table in Born & Wolf, and it's actually not particularly good--the peak should be 555nm instead on 560nm (but this makes it easier to use and is more than sufficient for your purposes). Additionally, it is the photopic ("bright light") luminosity curve; I don't have any data on the scotopic ("feeble light") curve, which would be more applicable here, other than its peak being 507nm. The overall shape is nearly identical to the photopic one (from Fig. 4.32 in B&W 3rd ed.). It's probably adequate to simply move the peak from 560 to 507.Destructionator XIII wrote:2) What energy number would be reasonable for a telescope or other sensor, including the naked eye to see something standing out? What emissivity number would be a reasonable estimate for a spaceship or its reaction mass?
One method of comparison would be to calculate the luminosity flux of the sun. Using the above method, except with a cubic rather than quadratic interpolation in logs, the output of the Sun comes out to be 3.3e28 lumens, or 1.2e5 lux (lum/m²) at 1AU, ignoring atmospheric effects. If this corresponds to an apparent magnitude of about -26.7 at 1AU, then an object of apparent magnitude 5 would deliver 2.5e-8 lux; this represents just about the faintest of objects visible with the naked eye, give or take a factor of three, depending on local light pollution, etc. The same analysis would apply to all optical telescopes, except that they are capable of seeing fainter objects.
Of course not. I suppose one way to attempt to quantify it would be to calculate the spectral difference between the background and object, which would automatically account for both raw luminosity differences and color differences. Unfortunately, I'm not familiar enough with photometry to present more than guesses on this matter. Perhaps there is a better way to answer the previous question as well.Destructionator XIII wrote:3) How would this change if there was something in the background, such as if Earth was behind the ship? Would it still be as easily seen?
Edit: exp[-(λ-560.3)²/60.64²], not exp[-(λ-560.3)/60.64²].