Question #58092

The change in the value of acceleration of earth towards sun, when the moon comes from the position of solar eclipse to the position on the other side of earth in line with the sun is? (mass of moon = 7.36 × 〖10〗^22 kg, orbital radius of moon = 3.8 ×〖10〗^8 m)
1

Expert's answer

2016-03-09T09:04:05-0500

Answer on Question 58092, Physics, Astronomy, Astrophysics

Question:

The change in the value of acceleration of Earth towards Sun, when the Moon comes from the position of solar eclipse to the position on the other side of Earth in line with the Sun is? (mass of Moon is 7.361022kg7.36 \cdot 10^{22} kg , orbital radius of Moon is 3.82108m3.82 \cdot 10^{8} m )

Solution:

Let's draw, for clarity, the free-body diagrams for Earth in the two situations (solar eclipse and lunar eclipse):



Here, FSF_{S} is the magnitude of the gravitational attraction of the Sun on Earth, FMF_{M} is the magnitude of the gravitational attraction of the Moon on the Earth. It is obvious, that the magnitudes of the net forces acting on the Earth are FS+FMF_{S} + F_{M} in case of a solar eclipse and FSFMF_{S} - F_{M} in case of a lunar eclipse.

Let's write the forces FSF_{S} and FMF_{M} using the Newton's Law of Universal Gravitation:


FS=GMSMEDS2,FM=GMMMEDM2,F _ {S} = G \frac {M _ {S} M _ {E}}{D _ {S} ^ {2}}, F _ {M} = G \frac {M _ {M} M _ {E}}{D _ {M} ^ {2}},


here, GG is the universal gravitational constant, MSM_S is the mass of the Sun, MEM_E is the mass of the Earth, MMM_M is the mass of the Moon, DSD_S is the distance from the Earth to the Sun, DMD_M is the distance from the Earth to the Moon.

It is obviously, that the net forces acting on the Earth in cases of the solar eclipse and the lunar eclipse are balanced by the Earth's acceleration MEaM_{E}a :


MEaS=F=FS+FM,MEaL=F=FSFM,M _ {E} a _ {S} = \sum F = F _ {S} + F _ {M}, M _ {E} a _ {L} = \sum F = F _ {S} - F _ {M},MEaS=GMSMEDS2+GMMMEDM2,MEaL=GMSMEDS2GMMMEDM2,M _ {E} a _ {S} = G \frac {M _ {S} M _ {E}}{D _ {S} ^ {2}} + G \frac {M _ {M} M _ {E}}{D _ {M} ^ {2}}, \qquad M _ {E} a _ {L} = G \frac {M _ {S} M _ {E}}{D _ {S} ^ {2}} - G \frac {M _ {M} M _ {E}}{D _ {M} ^ {2}},aS=G(MSDS2+MMDM2),aL=G(MSDS2MMDM2),a _ {S} = G \left(\frac {M _ {S}}{D _ {S} ^ {2}} + \frac {M _ {M}}{D _ {M} ^ {2}}\right), a _ {L} = G \left(\frac {M _ {S}}{D _ {S} ^ {2}} - \frac {M _ {M}}{D _ {M} ^ {2}}\right),


here, aSa_{S} is the acceleration of Earth in case of the solar eclipse, aLa_{L} is the acceleration of Earth in case of the lunar eclipse.

Then, we can find the change in the value of acceleration of Earth towards Sun, when the Moon comes from the position of solar eclipse to the position on the other side of Earth in line with the Sun:


aS=G(MSDS2+MMDM2)=6.671011Nm2kg2(1.991030kg(1.501011m)2+7.361022kg(3.82108m)2)=0.00593288ms2.\begin{array}{l} a_{S} = G \left(\frac{M_{S}}{D_{S}^{2}} + \frac{M_{M}}{D_{M}^{2}}\right) = 6.67 \cdot 10^{-11} \frac{N \cdot m^{2}}{kg^{2}} \cdot \left(\frac{1.99 \cdot 10^{30} kg}{(1.50 \cdot 10^{11} m)^{2}} + \frac{7.36 \cdot 10^{22} kg}{(3.82 \cdot 10^{8} m)^{2}}\right) \\ = 0.00593288 \frac{m}{s^{2}}. \end{array}aL=G(MSDS2MMDM2)=6.671011Nm2kg2(1.991030kg(1.501011m)27.361022kg(3.82108m)2)=0.0058656ms2.\begin{array}{l} a_{L} = G \left(\frac{M_{S}}{D_{S}^{2}} - \frac{M_{M}}{D_{M}^{2}}\right) = 6.67 \cdot 10^{-11} \frac{N \cdot m^{2}}{kg^{2}} \cdot \left(\frac{1.99 \cdot 10^{30} kg}{(1.50 \cdot 10^{11} m)^{2}} - \frac{7.36 \cdot 10^{22} kg}{(3.82 \cdot 10^{8} m)^{2}}\right) \\ = 0.0058656 \frac{m}{s^{2}}. \end{array}aSaL=0.00593288ms20.0058656ms2=0.0000673ms2=6.73105ms2.a_{S} - a_{L} = 0.00593288 \frac{m}{s^{2}} - 0.0058656 \frac{m}{s^{2}} = 0.0000673 \frac{m}{s^{2}} = 6.73 \cdot 10^{-5} \frac{m}{s^{2}}.


Answer:


aSaL=6.73105ms2.a_{S} - a_{L} = 6.73 \cdot 10^{-5} \frac{m}{s^{2}}.


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