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What Was The Potential Energy Of The Earth-spacecraft System?

Ten days after it was launched toward Mars in December 1998, the Mars Climate Orbiter spacecraft (mass 629 kg) was
2.87 x 10^6 km from the earth and traveling at
1.20 x 10^4 km/h relative to the earth.

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One Response to “What Was The Potential Energy Of The Earth-spacecraft System?”

  • shijiere says:

    Potential energy U = -GMm/r
    G = 6.67 x 10^-11 Mm^2/kg^2
    M = 5.98 x 10^24 kg
    m = 629 kg
    r = 2.87 x 10^9 m
    U = -8.7 x 10^7 J

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