What aero model are you using and how are you calculating the gravity turn
and angle of attack losses?
Or at this point are you just adding some margin to the delta v target
figure and just approximating?
On Sun, Jan 30, 2011 at 6:03 PM, Benjamin Kaplin <bkap...@pdx.edu> wrote:
>> - m_i1 Mass of 1st stage only, including fuel
>> - m_f2 Mass of 2nd stage only, excluding fuel
> This comment pointed out to me that the script was really only useful for
> designing a particular stage. So, to provide a more general tool, I rewrote
> the script. It should be a lot more user-friendly now. It allows for cool
> things like specifying the supportmass/fuelmass ratio on a per-stage basis.
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