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A spaceship of mass \(2 \times 10^4 kg\) is launched into a circular orbit close to the earth surface. The additional ve…

Q1

A spaceship of mass \(2 \times 10^4 kg\) is launched into a circular orbit close to the earth surface. The additional velocity to be imparted to the spaceship in the orbit to overcome the gravitational pull will be (if \(g=10 m / s ^2\) and radius of earth \(=6400 km )\)

a

\(
11.2(\sqrt{2}-1) km / s
\)

b

\(
7.9(\sqrt{2}-1) km / s
\)

c

\(
8(\sqrt{2}-1) km / s
\)

d

\(
7.4(\sqrt{2}-1) km / s
\)

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