## hyperbolic interplanetary transfer

Could someone tell me if I'm right or wong...

I want to calculate de hyperbolic excess speed for a spacecraft that leaves earth parking orbit on a hyperbolic orbit in direction to Jupiter to arrive there in optimum conditions.

It's not an Hohmann heliocentric transfer!!!

so, i though that:

$$v_{\infty} = v_{park} - v_{earth/jupiter}$$

Is it right, or is it worng?

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 Sorry, this tread can now be safely closed (and it only passed less than 10 min)... The hyperbolic velocity that I previosly wrote is totally wrong! In fact, $$v_{\infty} = \Delta v$$ where $$\Delta v$$ is the first impulse from the hohmann heliocentric transfer....

Recognitions:
 Quote by dilasluis Sorry, this tread can now be safely closed (and it only passed less than 10 min)... The hyperbolic velocity that I previosly wrote is totally wrong! In fact, $$v_{\infty} = \Delta v$$ where $$\Delta v$$ is the first impulse from the hohmann heliocentric transfer....