Hohmann transfer orbits (delta-v)

  • Thread starter Thread starter louischaman
  • Start date Start date
  • Tags Tags
    Delta-v Orbits
Click For Summary

Homework Help Overview

The discussion revolves around Hohmann transfer orbits, specifically focusing on the mathematical derivation of delta-v equations related to orbital mechanics. Participants are exploring the relationships between orbital velocities and radii in the context of space travel.

Discussion Character

  • Mathematical reasoning, Assumption checking, Problem interpretation

Approaches and Questions Raised

  • Participants are attempting to derive equations for delta-v using known relationships between orbital parameters. Some are expressing confusion over intermediate steps and algebraic manipulations, while others are questioning the assumptions behind the formulas being used.

Discussion Status

The discussion is ongoing, with participants sharing their attempts at algebraic manipulation and expressing difficulties in progressing further. Some guidance has been offered regarding algebraic techniques, but there is no clear consensus on the next steps or solutions.

Contextual Notes

Participants have noted challenges with using LaTeX for mathematical expressions and have mentioned the need for clarity on certain mathematical concepts related to the problem.

louischaman
Messages
3
Reaction score
0
I am writing an essay on Space travel for my A level coursework. I am writing about Hohmann transfer orbits.
At the moment I am using the wikipedia page:
http://en.wikipedia.org/wiki/Hohmann_transfer_orbit

It explains how you can derive this:
5944b27b3c44c602b17844e1ec4d3a0f.png


From this:

ec3f328abd4ffc5db4adb3c218da2544.png


I can't do the in between steps.
help would be appreciated
 
Physics news on Phys.org
I don't fully understand this either, and would like to know :P

However! I think the process would be;

v1² = u (2/r1 - 1/a )
v2² = u (2/r2 - 1/a )

with v1 v2 r1 r2 correponding to a velocity of X when you're in X orbit.

Anyway, i tried minusing them, and got into trouble :X, anyone help?
 
Well, consider delta v: delta v = v2 - v1.

Square that: (delta v)^2 = v2^2 - 2v2v1 + v1^2.

Now, from the original equation, v2 = sqrt(mu)sqrt(2/r2 - 1/a)
and v1 = sqrt(mu)sqrt(2/r1 - 1/a)
so -2v2v1 = -mu sqrt((2/r2 - 1/a)(2/r1 - 1/a))
and v2^2 = mu(2/r2 - 1/a)
and v1^2 = mu(2/r1 - 1/a)

so (delta v)^2 = mu(2/r2 - 1/a) - mu sqrt((2/r2 - 1/a)(2/r1 - 1/a)) + mu(2/r1 - 1/a)

Some algebra should get you to something that looks like the right side of the target equation. You'll probably need some tricks (partial fractions and similar) to force it into the right form.
 
]Hey there, thanks for the tip, however (and this is more maths related i guess) I'm having trouble getting there;

I've got to

delta v² = 2u [ 1/r1 + 1/r2 - 2/2a - sqrt(4/r1r2 - 2/r1a - 2/r2a + 1/a²)]

Really stuck on what to do next, I know what the answer is, but i can't seem to get rid of the a's :confused: any help would be appreciated, and yeah i need to learn how to use the proper formula thingy rather than just typing it out, any help there would be great too :P is it a separate program because the latex thing in advanced is useless
 
Last edited:
[tex]\Delta[/tex]v² = 2 [tex]\mu[/tex] [ [tex]\frac{1}{r1}[/tex] + [tex]\frac{1}{r2}[/tex] - [tex]\frac{2}{2a}[/tex] - [tex]\sqrt{\frac{4}{r1r2}[/tex]-[tex]\frac{2}{r1a}[/tex]-[tex]\frac{2}{r2a}[/tex]+[tex]\frac{1}{a^2}[/tex]

excuse my failure with latex, all of the last bit is suposed to be square rooted...however i can't work that out :P

I can't get any further from here :frown:
 
Hey, sorry for the bump but this is a really annoying problem =[
 

Similar threads

Replies
1
Views
1K
  • · Replies 2 ·
Replies
2
Views
1K
Replies
5
Views
3K
  • · Replies 4 ·
Replies
4
Views
3K
  • · Replies 1 ·
Replies
1
Views
7K
  • · Replies 1 ·
Replies
1
Views
2K
  • · Replies 1 ·
Replies
1
Views
3K
  • · Replies 1 ·
Replies
1
Views
4K
Replies
4
Views
5K
  • · Replies 1 ·
Replies
1
Views
2K