Comp forc by when it's at opposition. Express your result as a numerical fraction of the differential tidal force exerted by the Moon, AFM0on where ro= 384,000km = 0.00257AU is the Earth-Moon distance and MM9on= 7.2 < 1022kg is the mass of the Moon. Repeat to find the differential tidal force AF exerted by Jupiter at opposition, also expressed as a fraction of AEMoon: Assume that the Moon, Earth, Mars, and Jupiter are on circular coplanar orbits.)
Comp forc by when it's at opposition. Express your result as a numerical fraction of the differential tidal force exerted by the Moon, AFM0on where ro= 384,000km = 0.00257AU is the Earth-Moon distance and MM9on= 7.2 < 1022kg is the mass of the Moon. Repeat to find the differential tidal force AF exerted by Jupiter at opposition, also expressed as a fraction of AEMoon: Assume that the Moon, Earth, Mars, and Jupiter are on circular coplanar orbits.)
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
Transcribed Image Text:4.
Compute the differential tidal force AF exerted on the Earth by Mars
when it's at opposition. Express your result as a numerical fraction of the
differential tidal force exerted by the Moon,
2GMMoonm RO
where ro = 384,000km = 0.00257AU is the Earth-Moon distance and MMoon = 7.2
x 1022kg is the mass of the Moon. Repeat to find the differential tidal force AF
exerted by Jupiter at opposition, also expressed as a fraction of AEMaen.
(Assume that the Moon, Earth, Mars, and Jupiter are on circular coplanar
orbits.)
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