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The Helios B spacecraft had a speed of 71 km/s when it was

4.3km from the sun.
Prove that its orbit about the sun was closed
andtherefore eliptical.

User Marlos
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1 Answer

6 votes

Step-by-step explanation:

It is given that,

Speed of the spacecraft, v = 71 km/s = 71000 m/s

Distance between the spacecraft and the Sun,
d = 4.3* 10^7\ km = 4.3* 10^(10)\ m

It is required to proof that its orbit about the sun was closed and therefore elliptical. Let v is the speed with which the spacecraft if it is moving in circular path. It is given by :


v=\sqrt{(GM)/(r)}

M is the mass of the sun,
M=2* 10^(30)\ kg


v=\sqrt{(6.67* 10^(-11)* 2* 10^(30))/(4.3* 10^(10))}

v = 55698 m/s

or

v = 55.6 km/s

The given velocity is 71 km/s while the calculated value of velocity is 55.6 km/s. It is clear that the path is not circular. It is elliptical. Hence, this is the required solution.

User Rinat Diushenov
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