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The hyperbolic excess speed of a spacecraft is the excess velocity of the spacecraft at the exit of the sphere of influence of the planet. Which when we are on the ecliptic of the planet will be difference between the planets velocity on the ecliptic plane minus the speed of the spacecraft...

Hey guys, For a side project I'm making a study on the external thermal control systems of the ISS and am wondering what would be the best way to start off.

Hey guys, I am a Masters student in Space Engineering and my hands have been tied up with this question that I have encountered. Hope some of you guys can help me sort out this question. Q. A spacecraft reaches Mercury while travelling on a heliocentric orbit, co-planar with the Mercury orbit...