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**Unformatted text preview: **of the earth, moon and spacecraft is a solution of the Lagrange Circular Restricted Three-Body Problem. The spacecraft is at one of the earth-moon system Lagrange points. The Trojan asteriods are found at the corresponding Jovian Lagrange points. or , is work The b) m 10 3.84 kg) kg)(1250 10 35 . 7 kg 10 97 . 5 )( kg / m N 10 673 . 6 8 22 24 2 2 11 × × + × ⋅ ×--=-= r GMm W J. 10 31 . 1 9 ×-= W...

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