MetalMania
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I've been messing around with IMFD on and off for a while, tried a bunch of tutorials, read the "full manual", watched playbacks, etc. When I follow a tutorial, generally I have no problem. I think I understand the concepts and the basics of what does what, but when I try to use it on one of my own flights things don't go so well. At best I get where I'm trying to go but it's ugly, at worst I completely miss my target.
Most recently I've been having a go at "Jupiter Rockets (DIRECT)" by dougkeenan. I'm doing a "dual launch" scenario where I dock an Earth Departure Stage booster with a docked Orion crew vehicle and Lunar Module in LEO, and use the EDS to do a TLI burn. My RInc to the Moon in LEO is 0.5 degrees. Despite trying to follow the principles I've learned (or at least what I think I've learned) from tutorials etc, I either end up way short in my burn, miss the intercept with the Moon, or can't get my Lunar PeA as shown in the IMFD Map display raised from deep beneath the surface. Yes, I'm trying to do MCC burns. The last couple of times I've tried it I set up a burn in Target Intercept that at least should make it out to the Moon's orbit, yet the auto-burn cuts off well before my new orbit reaches that size. Which leads me to the title of this post.
Does IMFD account for the total mass of all components of a docked "stack"? I'm wondering if the burn is coming up short because it only considers the mass of teh EDS stage?
Just to try something different I tried with a DGIV, figuring I'll take the whole "stack mass" issue out and use a single vessel. Well, this time I tried to plot a course for a plain Jane prograde intercept, and ended up with AB burning well past the planned trajectory, and the map view now shows a free return figure 8. But if I tried for a free return, unless I was following an Apollo tutorial, I'd never get it to work.
I'm starting to feel like IMFD for me stands for "I aM F#$!^& Dumb".
Most recently I've been having a go at "Jupiter Rockets (DIRECT)" by dougkeenan. I'm doing a "dual launch" scenario where I dock an Earth Departure Stage booster with a docked Orion crew vehicle and Lunar Module in LEO, and use the EDS to do a TLI burn. My RInc to the Moon in LEO is 0.5 degrees. Despite trying to follow the principles I've learned (or at least what I think I've learned) from tutorials etc, I either end up way short in my burn, miss the intercept with the Moon, or can't get my Lunar PeA as shown in the IMFD Map display raised from deep beneath the surface. Yes, I'm trying to do MCC burns. The last couple of times I've tried it I set up a burn in Target Intercept that at least should make it out to the Moon's orbit, yet the auto-burn cuts off well before my new orbit reaches that size. Which leads me to the title of this post.
Does IMFD account for the total mass of all components of a docked "stack"? I'm wondering if the burn is coming up short because it only considers the mass of teh EDS stage?
Just to try something different I tried with a DGIV, figuring I'll take the whole "stack mass" issue out and use a single vessel. Well, this time I tried to plot a course for a plain Jane prograde intercept, and ended up with AB burning well past the planned trajectory, and the map view now shows a free return figure 8. But if I tried for a free return, unless I was following an Apollo tutorial, I'd never get it to work.
I'm starting to feel like IMFD for me stands for "I aM F#$!^& Dumb".