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Exercises · 7.19

Q.A satellite orbits the earth at a height of 400 km above the surface. How much energy must be expended to rocket the satellite out of the earth's gravitational influence? Mass of the satellite =200 kg= 200\text{ kg}; mass of the earth =6.0×1024 kg= 6.0 \times 10^{24}\text{ kg}; radius of the earth =6.4×106 m= 6.4 \times 10^{6}\text{ m}; G=6.67×10−11 N m2 kg−2G = 6.67 \times 10^{-11}\text{ N m}^{2}\text{ kg}^{-2}.

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A satellite in a circular orbit has total mechanical energy E=−GMm2rE=-\dfrac{GMm}{2r}; sending it out of Earth's gravitational influence means raising this to zero, so the energy required equals ∣E∣|E|. For this satellite, that works out to about 5.89×1095.89\times10^9 J.

Setting up

The satellite orbits at height 400 km, so its distance from Earth's centre is

r=R+h=6.4×106+4.0×105=6.8×106 mr = R+h = 6.4\times10^6+4.0\times10^5 = 6.8\times10^6\text{ m}

Total energy in the orbit

For a circular orbit, kinetic energy is exactly half the magnitude of the potential energy, so the total mechanical energy is

E=−GMm2rE = -\frac{GMm}{2r}

with M=6.0×1024M=6.0\times10^{24} kg, m=200m=200 kg, G=6.67×10−11G=6.67\times10^{-11} N m2^2 kg−2^{-2}:

GMm=(6.67×10−11)(6.0×1024)(200)=8.004×1016GMm = (6.67\times10^{-11})(6.0\times10^{24})(200) = 8.004\times10^{16}

E=−8.004×10162×6.8×106=−8.004×10161.36×107≈−5.89×109 JE = -\frac{8.004\times10^{16}}{2\times6.8\times10^6} = -\frac{8.004\times10^{16}}{1.36\times10^7} \approx -5.89\times10^9\text{ J}

Energy needed to escape …

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