A 1400 kg spacecraft is 3 Earth radii above the Earth’s surface. What is the acceleration due to gravity at this distance above the earth
using Newton's second law we get the acceleration of gravity at
the planet's surface:
a = F/m = {F = G(m1m2)/(r2)}/m2 = G(m1)/(r2)
so the acceleration of gravity at
the surface is:
a = G(m1)/(r2)
I will use 6.38x106m as the radius of the earth, so this planet has
a radius of 3*(6.38x106m) = 1.914x107m
Earth has a mass of 5.98x1024kg, and so let's just plug this into
our equation:
a = (6.67x10-11 Nm2/kg2)(5.98x1024 kg)/(1.914x107m)2 =
1.088 m/s2
a = 1.1 m/s2
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