1.

A spaceship is launched into a circular orbit of radius R close to the surface of the earth. The additional velocity to be imparted to the spaceship in the orbit to overcome the earth.sgravitationalpull is (g to accelerationdue to gravity)

Answer»

`1.414 RG`
`1.414 SQRT(GR)`
`0.414 Rg`
`0.414 sqrt(gR)`

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