At a certain instant, the earth, the moon, and a stationary 1450kg spacecraft lie at the vertices of an equilateral triangle whose sides are 3.84
a) gravitational force =Gm1m2/r^2
mass of earth=5.97*10^24 kg
F = 6.673*10^-11*5.97*10^24*1450 / (3.84*10^5)^2
F = 3.92*10^6 N
b) gravitational force between the moon and the spacecraft = 6.673*10^-11*7.34*10^22*1450 / (3.84*10^5)^2
= 48164N
angle between the force exerted by the moon and the force exterted by the earth is 60
So Fnet = sqrt(F1^2+F2^2 + 2F1F2cos a)
Fnet = sqrt ( (3.92*10^6)^2 + 48164^2 + 2*3.92*10^6*48164*cos 60 )
Fnet = 3.94*10^6N
c) minimum work needed = total energy of the two positions
Work done = E(final)-E(initial)
W= GM/r (Mearth- Mmoon)
W= 6.67*10^-11*1450 / 3.84*10^5 * ( 5.97*10^24 - 7.34*10^22)
W=1.48*10^12J
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