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^2d=ut+21at2
where:
- ddd is the distance traveled,
- uuu is the initial velocity (which is zero in this case as the spaceship starts from rest),
- aaa is the acceleration, and
- ttt is the time.
In this case, the spaceship's acceleration is given as a=150 m/s2a = 150 , ext{m/s}^2a=150m/s2 and the distance to the asteroid is d=1.2 km=1200 md = 1.2 , ext{km} = 1200 , ext{m}d=1.2km=1200m.
Plugging these values into the equation, we get:
1200=0⋅t+12⋅150⋅t21200 = 0 cdot t + frac{1}{2} cdot 150 cdot t^21200=0⋅t+21⋅150⋅t2
Simplifying the equation, we have:
1200=75t21200 = 75t^21200=75t2
Dividing both sides by 75, we get:
16=t2<annotation e