Engineering HW Help

montecarlo01ss

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2rfvofb.jpg

any ideas?
 

montecarlo01ss

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haha its for aerospace engineering, not my major but its a introduction course to all the engineering majors so i have to do it
 

cobra_matt

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Case 1, I got 9210.340 m/s.
Case 2, I got 92103.404 m/s.

Edit: First time I did it, I used Mfinal / Minitial = 0.9, but that doesn't make sense since the propellant is burned off leaving 10% of the initial mass left. But the delta V sounds really high, so take my solution with a grain of salt.
 
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black4vcobra

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Case 1, I got 421.442 m/s.
Case 2, I got 4214.421 m/s.

Ditto, pretty basic stuff here.. You have to multiply by the natural log function (LN) on your calculator for both sides of the equation .9=e^(-delta v/U).

LN*.9 = LN*e^(-delta V/ U)

LN*e^(x/y) = (x/y)

Edit: as pointed out, .1 is the ratio to use, not .9
 
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MrSwa

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It depends on how you read the problem.
If M_f = 0.9*M_i then 0.9*M_i/M_i = 0.9, but if it means that 90% was used up, then bkaul is right with the 0.1 (or 10%). I would lean toward 0.1 after looking closer at it. Good luck.
 

speedofsound

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For propulsion, that equation is what F=ma is to physics. I just had flashbacks ...thanks.
 
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jmk97GT

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Case 1, I got 9210.340 m/s.
Case 2, I got 92103.404 m/s.

Edit: First time I did it, I used Mfinal / Minitial = 0.9, but that doesn't make sense since the propellant is burned off leaving 10% of the initial mass left. But the delta V sounds really high, so take my solution with a grain of salt.

Yeah, that's correct...
 

Chris _Scott

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I'm trying to decide as to why I clicked on this thread...

As if I don't have enough of Engineering homework I have to do myself..
 

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