It has been a year or two since I last flew orbiter and I wanted to try something a bit more complex, and noticed the apparently-new interplantary MFD. However, much of the documentation is fairly old - I could only find one tutorial that references the current version. As an added bonus this will be my first attempt at a slingshot.
I want to fly Earth-Venus-Jupiter, and using the trajectory optimizer I have dates for my launch window.
Right now I'm still stuck on the ground about 18 hours before my departure time trying to set up. I was able to set up a course to Venus with an arrival date corresponding to my intercept date. Beyond that I've been fumbling around with Orbit-eject, but that was based on what appears to be outdated documentation. It sounds like I should skip that program and go straight to surface launch, but in that program it just says no valid course when I select the course mode. Am I missing something obvious?
I'll go ahead and outline my meager understanding of what I need to do after launch so that you can correct any issues while you're reading:
1. After launch I'll be in an orbit aligned to my departure (hopefully). At that point I load up the orbit-eject program, wait until my optimized departure time, then at the next window do the prograde burn (or just hit autoburn I assume).
2. Once outside the Earth SOI I use the planet approach program to set the altitude and inclination in the report generated by trajectory optimizer.
3. Once inside the Venus SOI I use the course program to plot a course to arrive at Jupiter at the optimized target date, and then use the orbit eject program to calculate the burn and run it.
4. At that point I'm just flying to Jupiter - I can use Planet approach or the tool of my choice to go from there.
I'll just use off-axis mode for now, but to do better it looks like I could correct inclination at a node rather than at launch.
Is that about right? I see a slingshot program but looking at the only docs I could find it seems like that is mainly informational.
---------- Post added at 02:01 PM ---------- Previous post was at 12:32 PM ----------
Hate to self-reply, but one other question. In the output report of the trajectory optimizer, which inclination is the one to use when inserting into orbit around Venus? I have two legs, each with an inclination. I'm not sure if leg1 is the departure from earth, or the arrival at Venus. Granted, the inclinations are only a few degress apart so I could probably recover mid-course if wrong.
And of course it is entirely possible I've got something fundamental wrong to begin with.
Oh, the details in case anybody needs to know:
Depart Earth 24-Apr-2015 9:56, Venus 9-Oct-2015 11:04, arrive Jupiter 15-Dec-2017 14:05. c3 is 15.53, delV is 110 - I couldn't find any place with ship stats to get a sense of whether those figures are reasonable, but they're smaller than the figures for a direct transfer so I guess they must be. (Flying the XR-5 - if it turns out the fuel just isn't sufficient I can always try again in something smaller but the XR-2 won't carry that much O2.)
I want to fly Earth-Venus-Jupiter, and using the trajectory optimizer I have dates for my launch window.
Right now I'm still stuck on the ground about 18 hours before my departure time trying to set up. I was able to set up a course to Venus with an arrival date corresponding to my intercept date. Beyond that I've been fumbling around with Orbit-eject, but that was based on what appears to be outdated documentation. It sounds like I should skip that program and go straight to surface launch, but in that program it just says no valid course when I select the course mode. Am I missing something obvious?
I'll go ahead and outline my meager understanding of what I need to do after launch so that you can correct any issues while you're reading:
1. After launch I'll be in an orbit aligned to my departure (hopefully). At that point I load up the orbit-eject program, wait until my optimized departure time, then at the next window do the prograde burn (or just hit autoburn I assume).
2. Once outside the Earth SOI I use the planet approach program to set the altitude and inclination in the report generated by trajectory optimizer.
3. Once inside the Venus SOI I use the course program to plot a course to arrive at Jupiter at the optimized target date, and then use the orbit eject program to calculate the burn and run it.
4. At that point I'm just flying to Jupiter - I can use Planet approach or the tool of my choice to go from there.
I'll just use off-axis mode for now, but to do better it looks like I could correct inclination at a node rather than at launch.
Is that about right? I see a slingshot program but looking at the only docs I could find it seems like that is mainly informational.
---------- Post added at 02:01 PM ---------- Previous post was at 12:32 PM ----------
Hate to self-reply, but one other question. In the output report of the trajectory optimizer, which inclination is the one to use when inserting into orbit around Venus? I have two legs, each with an inclination. I'm not sure if leg1 is the departure from earth, or the arrival at Venus. Granted, the inclinations are only a few degress apart so I could probably recover mid-course if wrong.
And of course it is entirely possible I've got something fundamental wrong to begin with.
Oh, the details in case anybody needs to know:
Depart Earth 24-Apr-2015 9:56, Venus 9-Oct-2015 11:04, arrive Jupiter 15-Dec-2017 14:05. c3 is 15.53, delV is 110 - I couldn't find any place with ship stats to get a sense of whether those figures are reasonable, but they're smaller than the figures for a direct transfer so I guess they must be. (Flying the XR-5 - if it turns out the fuel just isn't sufficient I can always try again in something smaller but the XR-2 won't carry that much O2.)