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To determine the time it takes for the spaceship to reach a distant asteroid, we can use the kinematic equation:

d=ut+12at2d = ut + frac{1}{2}at^2

where:

  • dd is the distance traveled,
  • uu is the initial velocity (which is zero in this case as the spaceship starts from rest),
  • aa is the acceleration, and
  • tt is the time.

In this case, the spaceship's acceleration is given as a=150 m/s2a = 150 , ext{m/s}^2 and the distance to the asteroid is d=1.2 km=1200 md = 1.2 , ext{km} = 1200 , ext{m}.

Plugging these values into the equation, we get:

1200=0⋅t+12⋅150⋅t21200 = 0 cdot t + frac{1}{2} cdot 150 cdot t^2

Simplifying the equation, we have:

1200=75t21200 = 75t^2

Dividing both sides by 75, we get:

16=t2<annotation e

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