What is the final velocity of a rocket propelled into space with a net acceleration of 200m/s^2 as it reaches an altitude of 10.0km? (Assuming an initial velocity of zero) ***thank you!!
Is this kinematics, or energy?
more kinematics:)
First look at velocity: \[ v(t)-v(0) = \int_0^ta(x)~dx = \int_0^t200(m/s^2)~dx = 200(m/s^2)\bigg|_{x=0}^{x=t} \]Initial velocity is zero, meaning \(v(0)=0\). We end up with:\[ v(t) = 200t(m/s^2) \]
Now we need to find \(t_f\), which is the time it reaches that high altitude.
okay:)
\[ x(t_f)-x(0) = \int_0^{t_f}200t(m/s^2)~dt = 200\frac{t^2}{2}(m/s^2)\bigg|_{t=0}^{t=t_f} \]We know that \(x(t_f)-x(0)=10.0(km)\) since that was its increase in altitude. So we get: \[ 10.0(km) =200\frac{(t_f)^2}2(m/s^2) \]We can use this to solve for \(t_f\).
ohh okay, so from here, would I first multiply by 2 on both sides? 20.0 (km)=200(tf)^2 ?
Yeah
and then now, divide by 200? 0.1= tf^2 ?
and square and get tf=0.316 ?
Yes, but remember your units. \[ 0.1(km) = t_f^2(m/s^2) \]
ahh right!! okay, and then tf=0.316 km/s/s^2 ?
Hold on, what units should \(t_f\) be in?
m/s^2 ?
Nope.
ohh darn :( not sure!! km?
First divide both sides by the units. \[ \frac{0.10(km)}{(m/s^2)}=t_f^2 \]
okay, so 0.10 km = t^f(m/s^2) ?
Remember that \(1km = 1000m\)
so 100 m = tf^2(m/s^2) ?
Yeah \[ 100m = t_f^2(m/s^2) \]First divide by \(m\) to get: \[ 100 = t_f^2(1/s)^2 \]Then multiply by \(s^2\) to get: \[ 100(s^2)=(t_f)^2 \]Then you take the square root.
ahhh okie:) and then we get tf=10 ?
\[ t_f=10(s) \]
ohh okay:) and so that would be the final velocity? :O
Then we need to put that into our equation we got for velocity:\[ v(t) = 200t(m/s^2) \]
\[ v_f=v(t_f) = 200(10(s))(m/s^2) \]
oh! okay:) and that's the final velocity? :O plug in and done? :O
Simplify it.
so we get 2000 m/s ?
@wio? did i simplify that correctly? would 2000 m/s be the final velocity?
I think so.
okie!! yay! thank you very much!! :D
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