Distance between the asteroid and spacecraft which will be given as -
| | = (x2 - x1)2 + (y2 - y1)2 + (z2 - z1)2
| | = [(9 x 105 m) - (3 x 105 m)]2 + [(-3 x 105 m) - (4 x 105 m)]2 + [(-17 x 105 m) - (-3 x 105 m)]2
| | = 2.81 x 1012 m2
| | = 1.67 x 106 m
The unit vector can be calculated by -
= / | |
= (x2 - x1) + (y2 - y1) + (z2 - z1) / (x2 - x1)2 + (y2 - y1)2 + (z2 - z1)2
= [(9 x 105 m) - (3 x 105 m)] + [(-3 x 105 m) - (4 x 105 m)] + [(-17 x 105 m) - (-3 x 105 m)] / (1.67 x 106 m)
= (6 x 105 m) + (-7 x 105 m) + (-14 x 105 m) / (1.67 x 106 m)
= (0.359) + (-0.419) + (-0.838)
(a) The force acting on the spacecraft which will be given by -
net = {G M m / | |2 }
where, M = mass of a spacecraft = 1200 kg
m = mass of an asteroid = 7 x 1015 kg
G = gravitational constant = 6.67 x 10-11 Nm2/kg2
then, we get
net = { [(6.67 x 10-11 Nm2/kg2) (1200 kg) (7 x 1015 kg)] / (2.81 x 1012 m2) } [(0.359) + (-0.419) + (-0.838) ]
net = (1.99 x 10-4 N) [(0.359) + (-0.419) + (-0.838) ]
net = (7.14 x 10-5 N) + (-8.33 x 10-5 N) + (-1.66 x 10-4 N)
Then, we have
net = < 7.14 x 10-5 , -8.33 x 10-5 , -1.66 x 10-4 > N
Problem 3.27 Your answer is incorrect. Try again At t = 484 s after midnight, a...
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