Jump to content

bi-elliptic transfer to GKO


Recommended Posts

Does anyone have experience of using a bi-ellptic transfer to get into GKO. In theory it shoiuld be more efficent that a Hohmann transfer, but I have not yet done the maths to see if it is worth the effort. Presumably it is really hard to get the timing right.

Link to comment
Share on other sites

Bi-elliptic transfer is only worthwhile when semimajor axis of the target orbit is at least 12 times larger or smaller than the starting orbit's and still the saved delta-v is only marginal. There's no problem with timing. You raise your apoapsis as high as you are willing to go (because it takes time), brake/accelerate at that apoapsis to get the periapsis to the required height, then brake at periapsis to get apoapsis back to where you need it.

Theoretical optimum is so-called biparabolic transfer, where you raise your apoapsis just to the escape velocity, then go to the apoapsis at infinity, there perform burn of 0 dv to adjust the periapsis, and after returning from infinity to the periapsis brake again to adjust the apoapsis. The only downside of biparabolic transfer is that it takes infinite time.

Link to comment
Share on other sites

^ In layman's terms:

Your probably better off going with just the hohmann transfer (faster, easier to comprehend, less burns/maneuvers, etc). Or even better, launching into a suborbital trajectory, circularize your orbit, but don't stop burning, keep going until Apoapsis is at GKO, ride to Ap (or just before it), than circularize. Done, and in less time and with less maneuvers than the standard get-orbit-then-boost and/or bi-elliptic.

Link to comment
Share on other sites

If you're going for a geosynchronous orbit around Kerbin, use a Hohmann transfer. Apoapsis or periapsis doesn't matter - just pick one.

Right now I'm going for a heliosynchronous orbit as part of the Constellation Program Challenge and I'm using a bi-elliptic transfer. So far it's used maybe 2,500 m/s of delta-V (with the bulk of that needed to boost the probe's apoapsis up to Jool's orbit, the rest of it to lower the periapsis to the target zone). Haven't done the third burn yet, so I couldn't tell you if there will ultimately any delta-V savings or not.

I'm like Kashua; not sure which target you're talking about here.

Link to comment
Share on other sites

Bi-elliptic transfer is only worthwhile when semimajor axis of the target orbit is at least 12 times larger or smaller than the starting orbit's and still the saved delta-v is only marginal. There's no problem with timing. You raise your apoapsis as high as you are willing to go (because it takes time), brake/accelerate at that apoapsis to get the periapsis to the required height, then brake at periapsis to get apoapsis back to where you need it.

Theoretical optimum is so-called biparabolic transfer, where you raise your apoapsis just to the escape velocity, then go to the apoapsis at infinity, there perform burn of 0 dv to adjust the periapsis, and after returning from infinity to the periapsis brake again to adjust the apoapsis. The only downside of biparabolic transfer is that it takes infinite time.

Dear Squad, please add an ∞X time acceleration so that we can play with relativistic concepts.

Link to comment
Share on other sites

This thread is quite old. Please consider starting a new thread rather than reviving this one.

Join the conversation

You can post now and register later. If you have an account, sign in now to post with your account.
Note: Your post will require moderator approval before it will be visible.

Guest
Reply to this topic...

×   Pasted as rich text.   Paste as plain text instead

  Only 75 emoji are allowed.

×   Your link has been automatically embedded.   Display as a link instead

×   Your previous content has been restored.   Clear editor

×   You cannot paste images directly. Upload or insert images from URL.

×
×
  • Create New...