1.

Let a planet revolving close to the earth, Obtain relation between escape speed and orbital speed.

Answer»

SOLUTION : `IMPLIES v_0 = SQRT((GM_e)/R_e)` and ESCAPE SPEED `ve= sqrt((24M_e)/R_e)`
`:. v_0/v_e=sqrt((GM_e)/R_exxR_e/(24M_e))`
`:. v_0/v_e=1/sqrt2 " or " v_e=sqrt2v_0`


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