Before the engines fail, the rocket's altitude at time <em>t</em> is given by
![y_1(t)=\left(80.6\dfrac{\rm m}{\rm s}\right)t+\dfrac12\left(3.90\dfrac{\rm m}{\mathrm s^2}\right)t^2](https://tex.z-dn.net/?f=y_1%28t%29%3D%5Cleft%2880.6%5Cdfrac%7B%5Crm%20m%7D%7B%5Crm%20s%7D%5Cright%29t%2B%5Cdfrac12%5Cleft%283.90%5Cdfrac%7B%5Crm%20m%7D%7B%5Cmathrm%20s%5E2%7D%5Cright%29t%5E2)
and its velocity is
![v_1(t)=80.6\dfrac{\rm m}{\rm s}+\left(3.90\dfrac{\rm m}{\mathrm s^2}\right)t](https://tex.z-dn.net/?f=v_1%28t%29%3D80.6%5Cdfrac%7B%5Crm%20m%7D%7B%5Crm%20s%7D%2B%5Cleft%283.90%5Cdfrac%7B%5Crm%20m%7D%7B%5Cmathrm%20s%5E2%7D%5Cright%29t)
The rocket then reaches an altitude of 1150 m at time <em>t</em> such that
![1150\,\mathrm m=\left(80.6\dfrac{\rm m}{\rm s}\right)t+\dfrac12\left(3.90\dfrac{\rm m}{\mathrm s^2}\right)t^2](https://tex.z-dn.net/?f=1150%5C%2C%5Cmathrm%20m%3D%5Cleft%2880.6%5Cdfrac%7B%5Crm%20m%7D%7B%5Crm%20s%7D%5Cright%29t%2B%5Cdfrac12%5Cleft%283.90%5Cdfrac%7B%5Crm%20m%7D%7B%5Cmathrm%20s%5E2%7D%5Cright%29t%5E2)
Solve for <em>t</em> to find this time to be
![t=11.2\,\mathrm s](https://tex.z-dn.net/?f=t%3D11.2%5C%2C%5Cmathrm%20s)
At this time, the rocket attains a velocity of
![v_1(11.2\,\mathrm s)=124\dfrac{\rm m}{\rm s}](https://tex.z-dn.net/?f=v_1%2811.2%5C%2C%5Cmathrm%20s%29%3D124%5Cdfrac%7B%5Crm%20m%7D%7B%5Crm%20s%7D)
When it's in freefall, the rocket's altitude is given by
![y_2(t)=1150\,\mathrm m+\left(124\dfrac{\rm m}{\rm s}\right)t-\dfrac g2t^2](https://tex.z-dn.net/?f=y_2%28t%29%3D1150%5C%2C%5Cmathrm%20m%2B%5Cleft%28124%5Cdfrac%7B%5Crm%20m%7D%7B%5Crm%20s%7D%5Cright%29t-%5Cdfrac%20g2t%5E2)
where
is the acceleration due to gravity, and its velocity is
![v_2(t)=124\dfrac{\rm m}{\rm s}-gt](https://tex.z-dn.net/?f=v_2%28t%29%3D124%5Cdfrac%7B%5Crm%20m%7D%7B%5Crm%20s%7D-gt)
(a) After the first 11.2 s of flight, the rocket is in the air for as long as it takes for
to reach 0:
![1150\,\mathrm m+\left(124\dfrac{\rm m}{\rm s}\right)t-\dfrac g2t^2=0\implies t=32.6\,\mathrm s](https://tex.z-dn.net/?f=1150%5C%2C%5Cmathrm%20m%2B%5Cleft%28124%5Cdfrac%7B%5Crm%20m%7D%7B%5Crm%20s%7D%5Cright%29t-%5Cdfrac%20g2t%5E2%3D0%5Cimplies%20t%3D32.6%5C%2C%5Cmathrm%20s)
So the rocket is in motion for a total of 11.2 s + 32.6 s = 43.4 s.
(b) Recall that
![{v_f}^2-{v_i}^2=2a\Delta y](https://tex.z-dn.net/?f=%7Bv_f%7D%5E2-%7Bv_i%7D%5E2%3D2a%5CDelta%20y)
where
and
denote final and initial velocities, respecitively,
denotes acceleration, and
the difference in altitudes over some time interval. At its maximum height, the rocket has zero velocity. After the engines fail, the rocket will keep moving upward for a little while before it starts to fall to the ground, which means
will contain the information we need to find the maximum height.
![-\left(124\dfrac{\rm m}{\rm s}\right)^2=-2g(y_{\rm max}-1150\,\mathrm m)](https://tex.z-dn.net/?f=-%5Cleft%28124%5Cdfrac%7B%5Crm%20m%7D%7B%5Crm%20s%7D%5Cright%29%5E2%3D-2g%28y_%7B%5Crm%20max%7D-1150%5C%2C%5Cmathrm%20m%29)
Solve for
and we find that the rocket reaches a maximum altitude of about 1930 m.
(c) In part (a), we found the time it takes for the rocket to hit the ground (relative to
) to be about 32.6 s. Plug this into
to find the velocity before it crashes:
![v_2(32.6\,\mathrm s)=-196\frac{\rm m}{\rm s}](https://tex.z-dn.net/?f=v_2%2832.6%5C%2C%5Cmathrm%20s%29%3D-196%5Cfrac%7B%5Crm%20m%7D%7B%5Crm%20s%7D)
That is, the rocket has a velocity of 196 m/s in the downward direction as it hits the ground.