The very POWERFUL the Solar Irradiated planet surface Rotational Warming Phenomenon: ( N*cp )^1/16

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.

A THOUGHT EXPERIMENT: let's compare Te.moon =270K with Tsat.io =110K

A THOUGHT EXPERIMENT

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Let's perform a thought experiment, let's suggest Moon is a heavy cratered planet, and therefore, Moon has Φ = 1;

It can be shown, Moon's (thought experiment) mean surface temperature would be then very much close to the Moon's effective temperature

Te.moon = 270K

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The comparison coefficient is:

[ (1-a) (1/R²) (N*cp)¹∕ ⁴ ]¹∕ ⁴

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Moon:

R = 1

a = 0,11

N = 0,0339 rotations/day

cp = 0,19 cal /gr.oC

Moon's comparison coefficient calculation:

[ (1-a) (1/R²) (N*cp)¹∕ ⁴ ]¹∕ ⁴

[ (1-0,11) (1²) (0,0339*0,19)¹∕ ⁴ ]¹∕ ⁴ =

[ (0,89) (1) (0,00641)¹∕ ⁴ ]¹∕ ⁴ = 

[ (0,89) (1) (0,2833) ]¹∕ ⁴ =

(0,25213)¹∕ ⁴ = 0,70861

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Io:

R = 5,20

1/R² = 1/5,2044² = 0,0369

a = 0,63

N = 0,5559 rotations/day

cp = 0,145 cal /gr.oC

Io's satellite measured mean surface temperature is

Tsat.io = 110K

Comparison coefficient calculation:

[ (1-a) (1/R²) (N*cp)¹∕ ⁴ ]¹∕ ⁴

[ (1-0,63) (1/5,2044²) (0,5559*0,145)¹∕ ⁴ ]¹∕ ⁴ =

[ (0,37) (0,0369) (0,08060)¹∕ ⁴ ]¹∕ ⁴ =

[ (0,37) (0,0369) (0,53283) ]¹∕ ⁴ =

(0,0072747)¹∕ ⁴ = 0,29205

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Let's proceed,

let's compare Te.moon =270K with Tsat.io =110K:

Te.moon /Tsat.io = 270K /110K = 2,4545

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Let's compare the Moon's and Io's comparison coefficients:

Coeff.moon /Coeff.io = 0,70861 /0,29205 = 2,4263

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2,4545 /2,4263 = 1,0116

or only 1,16% difference !!!

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Conclusion:

Everything is all right.

It is a demonstration of the Planet Surface Rotational Warming Phenomenon!

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Here it is the Table of data: Table 1. Comparison of Predicted (Tmean) vs. Measured (Tsat) Temperature for All Planets and moons in solar system.

Link:Also view Table 1

Also the

Table of contents - Links

0). Explain Rotational Warming Model.

1). The first steps.

2). The Initial PREMISE.

3).The Planetary Temperatures Comparison Criteria.

4). "The total amount of the specularly reflected portion of solar flux"

Link: Φ = 0,47 and FRESNEL

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.

11). The First Conclusions.

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.

12). Completed DeepSearch.

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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