We do the planets and moons surface temperatures comparison.
The presence of atmosphere doesn't warm Earth's surface.
It is the other reasons, not the presence of atmosphere, that make Earth warmer than the Moon by +68°C.
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Tsat.mean.io = 110 K
Let's calculate Io's effective temperature old blackbody equation:
Te.io = [ (1-a) So (1/R²) /4σ ]¹∕ ⁴
Τe.io = [ (1-0,63)1.362 W/m² *0.0369 /4*5,67*10⁻⁸ W/m²K⁴ ]¹∕ ⁴ =
= (81.990.238,1)¹∕ ⁴ = 95,16 K
There is a big difference of
110 K - 95,6 K = 14,4 °C
Tsat.mean.callisto = 134 K ± 11
Let's calculate Callisto's effective temperature old blackbody equation:
Te.callisto = [ (1-a) So (1/R²) /4σ ]¹∕ ⁴
Τe.callisto = [ (1-0,22)1.362W/m² *0.0369 /4*5,67*10⁻⁸ W/m²K⁴ ]¹∕ ⁴ =
= (172.844.285,7)¹∕ ⁴ = 114,66 K
Tsat.mean.callisto = 134 K ± 11
There is a big difference of
134 K - 114,66 K = 19,34 °C
So Callisto is warmer, no matter what.
Callisto is at the outmost distance from the Jupiter, so it cannot be warmed from the planet's IR, also because of the distance it has the lowest tidal effect.
But here it is what happens:
Callisto has (1 - 0,22) = 0,78 and Io has (1 - 0,63) = 0,37
That means Callisto "absorbs" twice as much solar energy
Callisto rotates 10 times less than Io, but Callisto has cp =1,
which is bid when compared to Io having cp = 0,145
Thus the (β*N*cp)¹∕ ⁴ for Calisto is (150*0,0599 *1)¹∕ ⁴ = 1,7313
does not differ much from the (β*N*cp)¹∕ ⁴ for Io, which is (150*0,5559 *0,145)¹∕ ⁴ = 1,8647
Io coefficient is ( 0,37 * 1,8647 )¹∕ ⁴ = 0,6899¹∕ ⁴ = 0,91137
Callisto coefficient is ( 0,78 * 1,7313 )¹∕ ⁴ = 1,3504¹∕ ⁴ = 1,07799
Callisto coeff /Io coeff = 1,07799 /0,91137 = 1,1828
Tsat.mean.callisto /Tsat.mean.io = 134 K /110 K = 1,2181
1,2181 /1,1828 = 1,029 or only 2,9 % difference !
Also the Io and Callisto have Φ = 1, when Europa and Ganymede have Φ = 0,47
So, all that together explains the reasons Callisto is the warmest Jupiter's satellite.
Table of contents - Links
0). Explain Rotational Warming Model.
3).The Planetary Temperatures Comparison Criteria.
4). "The total amount of the specularly reflected portion of solar flux"
5). How A Planet Retains The Solar Energy - the role of the Immediate IR emission.
6). Φ -Factor is an analogue of the well known Drag Coefficient Cd=0,47
7). “What ‘portion’ of ‘sunlight’ reaches surface of Earth?”
8). The satellites do not measure Bond Albedo.
9). Stefan-Boltzmann formula J = σ T4 W/m² doesn't apply to terrestrial temperatures.
10). The Theoretical Equation.
12). The actual reason of the observed Global Warming.
13). The Axial Precession's role in Global Warming.
14). The Original Milankovitch cycle.
15). The Reversed Milankovitch cycle.
16). The higher CO2 content in ice core samples relates to colder periods.
17). Sensible Heat /Latent Heat ratio.
18). The conventional greenhouses, and the role of immediate IR emission.
19). NASA Technical Memorandum An Earth Albedo Model
20). The yearly total Immediate IR Emitted solar energy - in our times - is lower.
21). The yearly total reflected solar energy - in our times - is lower.
Appendix - Links
1). Earth's Corrected Effective Temperature (210 K ) calculation.
2). Earth's Average Surface Temperature (288 K ) calculation.
3). Moon's Corrected Effective Temperature (224 K ) calculation.
4). Moon's Average Surface Temperature (220 K ) calculation.
5). Mars' Corrected Effective Temperature (174 K ) calculation.
6). Mars' Average Surface Temperature (210 K ) calculation.
7). Mercury's Corrected Effective Temperature (364 K ) calculation.
8). Mercury's Average Surface Temperature (340 K ) calculation.
9). Titan's Average Surface Temperature (93,7 K ) calculation.
10). Earth / Mars satellite measured mean surface temperatures 288 K and 210 K comparison.
11). Earth's /Moon's temps 288K /220K comparison.
13). Blog.
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The table of contents will be completed some time soon. For more pages view the menu at the top.
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