To solve this problem, we will use the following kinematic equation:
h = ut + (1/2)at^2
Where:
h = altitude
u = initial velocity (0 m/s, as the spacecraft is at rest)
a = acceleration
t = time
Given:
h = 450 m
t = 4.0 s
u = 0 m/s
a) To find the acceleration:
Using the given values in the equation, we get:
h = ut + (1/2)at^2
450 = 0 + (1/2)a(4.0)^2
450 = 8a
Divide both sides by 8 to isolate "a":
450/8 = a
a ≈ 56.25 m/s^2
Therefore, the spacecraft's acceleration is approximately 56.25 m/s^2.
b) To find the velocity:
We can use the formula for velocity:
v = u + at
Given:
u = 0 m/s
t = 4.0 s
a = 56.25 m/s^2
Substituting the values into the equation:
v = 0 + 56.25(4.0)
v ≈ 225 m/s
Therefore, the spacecraft is traveling at a velocity of approximately 225 m/s when it reaches an altitude of 450 m.
Within 4.0 seconds of liftoff, a spacecraft that is uniformly accelerating straight upward from rest reaches an altitude of 450 m [up].
a) What is the spacecraft’s acceleration?
b) At what velocity is the spacecraft travelling when it reaches this altitude?
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