http://img29.imageshack.us/img29/756/245cbbacfdd641de948bc38.png I need help with PART B It doesn't seem so complicated since it just conservation of momentum and energy but I'm missing the big picture. How should I set up the initial angular moment/energy and final angular momentum/energy?
Even I am trying. Let me go step by step and stop me wherever you have a doubt. We will solve it together
First let me assume r_p -->radius at perihilion r_a -->radius at aphilion
v_p -->velocity at perihilion v_a -->velocity at aphilion
Now, We know that angular momentum(L) is conserved L_p = (r_p)*(m)*(v_p) L_a = (r_a)*(m)*(v_a) L_p = L_a So we get (r_p)*(m)*(v_p) = (r_a)*(m)*(v_a) (r_p)(v_p)=(r_a)(v_a)
@Dumboy , understoood until here ??
yeah I got to that far but I'm stuck how I should combine that with energy equation..
Good, Now we must conserve energy. m_s → mass of sun m_sp -->mass of spacecraft Total energy at perihelion = Kinetic energy(K.E) of spacecraft + gravitational energy between spacecraft and sun = ½ * m* (v_p)^2 + G*(m_s) *(m_sp) / (r_p)^2 Total energy at aphilion = Kinetic energy(K.E) of spacecraft + gravitational energy between spacecraft and sun = ½ * m* (v_a)^2 + G*(m_s) *(m_sp) / (r_a)^2
m = m_sp
@Dumboy , any problems/doubt until here ??
are m_sp going to cancel out in the end? cause it's value is not given
yes :) You will see now
since total energy is conserved, we get ½ * m* (v_p)^2 + G*(m_s) *(m_sp) / (r_p)^2 = ½ * m* (v_a)^2 + G*(m_s) *(m_sp) / (r_a)^2 ½ * m* ( (v_p)^2 – (v_a)^2) = G*(m_s) *(m_sp) ( 1 / (r_a)^2 - 1/(r_p)^2 ) Since m = m_sp. ½ * ( (v_p)^2 – (v_a)^2) = G*(m_s) * ( 1 / (r_a)^2 - 1/(r_p)^2 )
@Dumboy , any problems/doubt until here ??
nope
Now use this relation we derived above from conservation of angular momentum (r_p)(v_p)=(r_a)(v_a) Therefore, (r_p)=(r_a)(v_a) / (v_p) Substitute this r_p in the equation by conservation of energy relation and tell me what you you get??
shouldn't we substitute one of the v's so we can get rid of one v?
Yes. Exactly that is what I was thinking. That's why I asked you to think from here
Good point :)
Yes you continue from here.. and tell me what you get?
I am facing a problem. I am getting square root of negative number. Same problem or you are getting the right answer??
I am getting v_p = sqrt(- 2*G*m_s)/r_p
??
I got to \[\sqrt{(2Gm_sr_p^2-2Gm_sr_a^2)/(r_p^2(r_a^2-r_p^2))}\] I'm sure how I could simplify this further..
not sure*
Take 2G_s common outstide. and cancel numerator and denominator but with a minus sign. You will get same answer as I got :(
@mos1635 , any help bro..
I meant you can provide any help :P
what do you mean by cancel numerator and denominator but with a minus sign?
\[\sqrt{2*G*m_S (r_p^2 -r_a^2)/ r_p^2(r_a^2 -r_p^2)}\] \[\sqrt{- 2*G*m_S/r_p^2 }\]
oh I see.. can you say G is -G since gravity acts downward and cancel out the negatives?
no way. There is some conceptual mistake @mos1635 , @apoorvk @Vincent-Lyon.Fr
@experimentX
gravitonial potensial energy does not need r^2 but r
Hi! The method described by shivam_bhalla is correct, but there is a mistake in the expression of the gravitational potential energy. GPE is not: GPE = + G*(m_s) *(m_sp) / (r_p)^2 but is (with minus sign): GPE = - G*(m_s) *(m_sp) / (r_p) <------- not squared
hawk eye @mos1635, and @Vincent-Lyon.Fr
@Dumboy , corect the mistake and check you are getting the right answer. I am also checking :)
I am getting it :) @Dumboy , hope you are getting the final answer too. @mos1635 and @Vincent-Lyon.Fr --> thanks for pointing out my blunder :P
you did all the work.nice job!!
I checked and it leads to the answers given in the problem.
Thanks :D. @Dumboy , please give the medal to @Vincent-Lyon.Fr . I cannot give more than 1 medal. @Dumboy , if you are having any problem, just tag me here. :)
yeah I got the answer too thank you for the help everyone :)
Welcome :)
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