Calculate Mass Exhausted Per Second from Space Shuttle Thrust

[tony873004]

At launch, the space shuttle’s engines develop 3.0 * 10^7 N of thrust. If the speed of the exhaust gasses is 15 km/s, what mass of gas is exhausted per second?

<br /> F=ma\Rightarrow m=\frac{F}{a}<br />

<br /> kg=\frac{kg\cdot m/s^2}{m/s^2}<br />

<br /> kg=\frac{kg\cdot m/s^{\rlap{--} {2}}}{m/s^{\rlap{--} {2}}}\Rightarrow <br /> m=\frac{3.0\cdot 10^7kg\cdot \rlap{--} {m}/\rlap{--} {s}}{15(\rlap{--} <br /> {k}\rlap{--} {m}/\rlap{--} {s})\ast 1000\rlap{--} {m}/\rlap{--} {k}\rlap{--} <br /> {m}}<br />

<br /> m=2000kg<br />

I'm not sure if I'm allowed to cancel out the squared part of s squared, and still associate the 3.0e7 N with units that no longer represent it. Is my answer even correct?

 

[dextercioby]

F=\frac{\Delta p}{\Delta t} =v\frac{\Delta m}{\Delta t}


That "Delta t" is obviously 1sec,since we're asked the flow in one second...

Therefore the mass exhausted in one second is:

\Delta m=\frac{F}{\frac{v}{\Delta t}}=...

Daniel.

P.S.That force corresponds to a loss in momentum in unit time.

 

[tony873004]

m=\frac{F}{\frac{\Delta v}{\Delta t}}=...
so...

m=F\frac{\Delta t}{\Delta v}

m=3*10^7kg(m/s^2)\frac{1s}{15000m/s}

m=2000 kg

Amazing I came up with the right answer anyway, because I think I could have been called for illegal use of units. Your way is more elegant. It make sense since this question is in the momentum chapter. Delta P in your example is change in momentum, right?

Thanks, Dex. You've bailed me out again

 

[dextercioby]

Sorry,it's the other way around with the variation of momentum.It's due to the mass flow,and not the velocity variation.I'll edit the post...

Daniel.