| | I thought I would do some orbital mechanics in VB because alot of people have acces to it thorough excel. Here is one I did to calculate the departure delta v for a hofmann transfer: CODE Function Hohmann_P(r1, r2, mu) Hohmann_P = Sqr(mu / r1) * Sqr(2 * r2 / (r1 + r2) - 1) End Function Okay that is overly simplistic. |


