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Planet approach. Set it up as early as possible, way outside the destination's SOI. Set the orbit altitude and inclination, then burn. Now wait till you get closer and burn again. Then once again inside the SOI. Now you can use Orbit Insert. It's automatic...

Very nice work, both content and production. I have an idea how much time it took you to produce that as I made a video for IMFD a while back: http://solo.dc3.com/orbiter/video/EuropaToCallisto/

Those with old computers and limited resources can always continue with Orbiter 2006. I laud Martin and the team for moving forward. I would have just bit the bullet and gone with VS 2008. Once making the break, the next stop should have as long a life as possible. To Urwumpe - warnings are...

This looks awesome. Thanks in advance for your creativity and hard work!

This looks awesome. A hearty thanks in advance for all your hard work and creativity!

Still having this problem. See attached image.

You might be interested in this one http://solo.dc3.com/orbiter/video/EuropaToCallisto/ It goes the other way, but you can see how to use IMFD to do such a Hohmann transfer...

I ran it with the default parameters, and when it finished, it displayed a giant icon with the label output.bmp in the center area. I right clicked and selected "activate contents" and it put a file output.bmp in the same folder as the exe. It looks like the plot, very nice! I'm looking...

Look at Acronis True Image Home 2009

I'm swamped with work, getting ready for a conference next week. When I return, I'll come back here and look. Feel free to email me at [email protected] to bug me too. This is intriguing. I'm very versed in C#.net and less so in VB.net, but I can work with it. I'd be happy to be a test subject, but...

Updated version of Chris Knestrick's Attitude MFD. This is version 3.0. Attitude MFD provides the user with attitude information (pitch, yaw, and roll) with respect to a pre-selected reference attitude. It also provides an "Attitude Hold" mode to automati

This MFD allows you to perform a precise approach to rendezvous with minimum fuel usage. It uses Hill's equations (also known as Clohessy-Wiltshire equations) to generate a desired approach profile based only on the interceptor's present position and a de