| 1- Rotation of Sun and planets |
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| By |
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| Sami Esmaeil * |
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| 2-Abstract. |
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| If a small body of
mass (m) orbits a large body of mass (M) then, may be we can calculate
the sidereal rotation period of the large body (M) |
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| by the rotational
equation. The rotational equation can calculate the rotation period for a
Star of mass (M) which circled by another mass (m). |
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| The
nine Planets orbit our sun so, we can calculate the rotation period
of our sun. Also, from the rotation Equation we can calculate the
rotation |
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| period of Earth,
Mars, Jupiter, Saturn, Uranus, Neptune and Pluto because all this planets are
circled by another moons. |
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| 3-Keywords. |
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| Rotation, Sun,
Planets, Moment, Inertia, Leap, Second, Mass, Radius |
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| 4-Main
text. |
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| 4-1-Introduction.: |
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| The moons are
"driving" the rotation of their parent planet in the same way, as
sun's rotation is being controlled by the planets. ( Franz J. Heeke;
Germany) . |
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| http://www.surf2000.de/user/f-heeke/article1.html |
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| There was a paper
published by the Astronomical Journal in April, 1965 (vol. 70, page 193) by
Paul D. Jose (Ref.2 ). |
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| He concluded that "Certain
forces exerted upon the Sun by the planets are the cause of the sunspot
cycle" . |
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| 4-2-The rotation Equation: |
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Equation (1) |
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| From
equation 1 and Kepler's laws: |
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Equation (2) |
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| Where: |
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| T=Sidereal rotation period of the large body (sec) |
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| K=Moment of inertia factor of the large body. |
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| G=Gravitational constant. |
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| M=Large body mass (kg) |
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| Re=
Equatorial radius for the large body (meter) |
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| a=Semimajor axis of the mass center of all satellites that orbit
large body (meter) |
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| m=Total mass of all satellites that orbit the large body (kg) |
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| re =Equatorial
radius of all satellites that orbit large body (meter) |
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| rp =Polar
radius of all satellites that orbit large body (meter) |
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| P=Rotation period of the moons's mass center
that orbit the large body (sec.) |
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| ----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
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| *Bsc, 1981
Mechanical engineering, Egypt, Email:
saeles@yahoo.com |
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| 4-3-Solar
system data sources. |
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| All
parameters according to NASA fact sheets (Ref.1) |
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| http://nssdc.gsfc.nasa.gov/planetary/factsheet/index.html |
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| 4-4-The
equation results: |
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| 4-4-1-Determination
of Earth rotation period: |
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| The Earth has one
satellite (the Moon) |
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| K=0.329865 |
current value =0.3308 |
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| M=5.9736E+24 (kg) |
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| Re= 6.3781E+6 (meter) |
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| a=3.844E+8 (meter) |
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| m=7.35E+22 (kg) |
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| re =1738100 (meter) |
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| rp =1736000 (meter) |
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| From the
rotation Equation, the rotation period of Earth=23.93 hr |
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| 4-4-2-The
Earth rotation is going to be faster: |
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| The Earth
rotation period is going to be faster as a result of increasing Earth- Moon
distance. |
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| From the
rotation equation, the Earth is fastening it's rotation period by -0.428 milliseconds/century (3.82
cm/year) |
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| A negative
leap second may be inserted every 233 000 year |
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| The lower
the rotation period of the large body, the higher the orbital one of it's
moon. |
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| The
rotation period was equal the orbital one= 54.7 hr at a distance of 73 500
000 meter, it is now 384 400 000 |
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| 4-4-3-Determination
of Mars rotation period: |
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| K=0.3581 |
current value =0.366 |
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| M=6.4185E+23 (kg) |
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| Re= 3397000 (meter) |
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| There are two
satellites orbit Mars |
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| m= Total mass of
all satellites that orbit the large body Mars (kg) |
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| = m1 (Phobos)+m2 (Deimos) =1.3E+16 |
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| a=semimajor axis
of the center of mass of all satellites that orbit Mars (meter) |
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| =(m1 a1
+m2 a2 )/(m1 +m2 )=1.1977E+7 (meter) |
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| re= Equatorial radius of the total
satellites (meter) |
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| re=[(r1)3+(r2)3]^0.3333=[(13400)3+(7500)3)]^0.3333=14128
(meter) |
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| rp= Polar radius of the total
satellites (meter) |
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| rp=[(r1)3+(r2)3]^0.3333=[(9200)3+(5200)3)]^0.3333=9714
(meter) |
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| From the
rotation Equation, the rotation period of Mars=24.62 hr |
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| 4-4-4-Mars
rotation is going to be slower: |
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| Mars rotation
period is going to be slower as a result of decreasing the distance of it's
moons' mass center. |
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| From the rotation
equation, Mars is slowing it's
rotation period by 0.67
second/century (1.8 meter/year) |
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| A positive 0.67
leap second may be inserted every 100 year |
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| The lower the
rotation period of the large body, the higher the orbital one of it's moon. |
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| The rotation
period was equal to the orbital one= 20.2 hr at a distance of 17 880 000
meter, it is now 12 000 000 |
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| 4-4-5-Determination
of Jupiter, Saturn, Uranus, Neptune, Pluto and sun rotation period: |
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| By the same way,
we can calculate their rotation periods from the rotation equation.(table-1) |
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| All moons of small
masses are negligible according to the equation results. |
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| 4-5-Conclusion: |
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| 1-The slower the
rotation period of the large body, the faster the orbital one of it's moon. |
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| 2-The slower the
rotation period of the large body, the smaller the distance of it's moon. |
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| 3-The slower the
rotation period of the large body, the higher it's density (D) |
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| 4-The slower the
rotation period of the large body, the smaller of it's moon density (d) |
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| 5-The slower the
rotation period of the large body, the smaller of it's moment of inertia
factor value (k) |
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| 6-Jupiter, Uranus
and Neptune may have the same moment of inertia factor approximately. |
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| 7-The moment of
inertia of Pluto is very close to that of Saturn. |
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| 5-Acknowledgements |
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| I express my
deep-felt gratitude to Meta Ottevanger, for helping me to compose this page |
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| Thanks to Franz J.
Heeke; (Germany) for his useful
internet web. |
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| Thanks to Jerald
Lee ; (USA) for his useful internet
discussion. |
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| 6-Appendix |
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| Title Rotation of sun and
planets |
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| AUTHOR Sami Esmaeil |
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| Keywords Rotation, Sun, Planets, Moment,
Inertia, Leap, Second, Mass, Radius |
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| 7-References |
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| 1-David R. Williams, 2006.
NASA Planetary fact sheet . |
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| http://nssdc.gsfc.nasa.gov/planetary/factsheet/index.html |
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| 2-Franz J.
Heeke, 2007 ,Shaker Effects in Celestial Mechanics |
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| http://www.surf2000.de/user/f-heeke/article1.html |
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3-Paul
D. Jose, 1965.Sun's Motion and Sunspots. The Astronomical Journal, Vol. 70,
Number 3, April 1965; P. 193-200
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| 9-Tables
and figures |
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Large body properties |
Small body properties |
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| Rotation |
Grav. |
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Equatorial |
Moment |
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Semi.Maj. |
Equatorial |
Polar |
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| Observed |
Calculated |
Const. |
Mass |
Radius |
of
inertia |
Mass |
Axis |
Radius |
Radius |
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| T |
G |
M |
Re |
K |
m |
a |
re |
rp |
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| hr |
hr |
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Kg |
meter |
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Kg |
meter |
meter |
meter |
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| Earth |
23.9345 |
23.9344 |
7E-11 |
6.0E+24 |
6.38E+06 |
0.329864 |
7.349E+22 |
3.84E+08 |
1.74E+06 |
1.74E+06 |
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| Moon |
7.35E+22 |
3.84E+08 |
1.74E+06 |
1.74E+06 |
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| Mars |
24.6230 |
24.6230 |
7E-11 |
6.4E+23 |
3.40E+06 |
0.358103 |
1.30E+16 |
1.20E+07 |
1.41E+04 |
9.72E+03 |
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| Phobos |
1.06E+16 |
9.38E+06 |
1.34E+04 |
9.20E+03 |
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| Deimos |
2.40E+15 |
2.35E+07 |
7.50E+03 |
5.20E+03 |
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| Jupiter |
9.9250 |
9.9354 |
7E-11 |
1.9E+27 |
71492000 |
0.257 |
3.93E+23 |
1.10E+09 |
3.47E+06 |
3.47E+06 |
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| Io |
8.93E+22 |
4.22E+08 |
1.82E+06 |
1.82E+06 |
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| Europa |
4.82E+22 |
6.71E+08 |
1.56E+06 |
1.57E+06 |
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| Ganymede |
1.48E+23 |
1.07E+09 |
2.63E+06 |
2.63E+06 |
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| Callisto |
1.08E+23 |
1.88E+09 |
2.41E+06 |
2.40E+06 |
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| Saturn |
10.656 |
10.6586 |
7E-11 |
5.7E+26 |
60268000 |
0.189 |
1.40E+23 |
1.23E+09 |
2.63E+06 |
2.62E+06 |
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| Enceladus |
1.08E+20 |
2.38E+08 |
2.56E+05 |
2.45E+05 |
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| Tethys |
6.18E+20 |
2.95E+08 |
5.36E+05 |
5.26E+04 |
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| Dione |
1.10E+21 |
3.77E+08 |
5.60E+05 |
5.60E+05 |
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| Rhea |
2.31E+21 |
5.27E+08 |
7.64E+05 |
7.64E+05 |
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| Titan |
1.35E+23 |
1.22E+09 |
2.58E+06 |
2.58E+06 |
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| Iapetus |
1.81E+21 |
3.56E+09 |
7.18E+05 |
7.18E+05 |
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| Uranus |
17.24 |
17.2380 |
7E-11 |
8.7E+25 |
25559000 |
0.2562 |
9.12E+21 |
4.24E+08 |
1.10E+06 |
1.10E+06 |
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| Miranda |
6.60E+19 |
1.29E+08 |
2.40E+05 |
2.33E+05 |
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| Ariel |
1.35E+21 |
1.91E+08 |
5.81E+05 |
5.78E+05 |
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| Umbriel |
1.17E+21 |
2.66E+08 |
5.85E+05 |
5.85E+05 |
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| Titania |
3.52E+21 |
4.36E+08 |
7.89E+05 |
7.89E+05 |
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| Oberon |
3.01E+21 |
5.84E+08 |
7.61E+05 |
7.61E+05 |
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| Neptune |
16.11 |
16.1088 |
7E-11 |
1.0E+26 |
24764000 |
0.2719 |
2.14E+22 |
3.55E+08 |
1.35E+06 |
1.35E+06 |
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| Triton |
2.14E+22 |
3.55E+08 |
1.35E+06 |
1.35E+06 |
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| Pluto |
153.292 |
153.2903 |
7E-11 |
1.25E+22 |
1195000 |
0.21528 |
1.62E+21 |
1.96E+07 |
5.93E+05 |
5.93E+05 |
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| Charon |
1.62E+21 |
1.96E+07 |
5.93E+05 |
5.93E+05 |
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| Sun |
609.12 |
609.1094 |
7E-11 |
2.0E+30 |
6.96E+08 |
0.059447 |
2.67E+27 |
1.13E+12 |
8.51E+07 |
7.88E+07 |
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| Mercury |
3.30E+23 |
5.79E+10 |
2.44E+06 |
2.44E+06 |
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| Venus |
4.87E+24 |
1.08E+11 |
6.05E+06 |
6.05E+06 |
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| Earth |
5.97E+24 |
1.50E+11 |
6.38E+06 |
6.36E+06 |
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| Mars |
6.42E+23 |
2.28E+11 |
3.40E+06 |
3.38E+06 |
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| Jupiter |
1.90E+27 |
7.79E+11 |
7.15E+07 |
6.69E+07 |
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| Saturn |
5.68E+26 |
1.43E+12 |
6.03E+07 |
5.44E+07 |
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| Uranus |
8.68E+25 |
2.87E+12 |
2.56E+07 |
2.49E+07 |
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| Neptune |
1.02E+26 |
4.50E+12 |
2.48E+07 |
2.43E+07 |
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| Pluto |
1.30E+22 |
5.91E+12 |
1.16E+06 |
1.15E+06 |
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| Table (1)
The rotation equation results and solar system parameters. |
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| Download the
full calculations from the Excel sheet |
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| http://www.geocities.com/saeles/Rotation.xls |
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