The escape velocity v a spacecraft needs to leave the gravitational field of a planet varies directly as the square root of the product of the planet’s radius R and its acceleration due to gravity g. For Mars and Earth:
Rm=.533 Re (e is small lower) and gm (m is small lower) =.400 ge(e is small lower)
Find vm(m is small lower) for Mars if the escape velocity for earth, Ve =11.2 km/s
Help!
Rm=.533 Re (e is small lower) and gm (m is small lower) =.400 ge(e is small lower)
Find vm(m is small lower) for Mars if the escape velocity for earth, Ve =11.2 km/s
Help!