- #1
dilasluis
- 32
- 0
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:
[tex] v_{\infty} = v_{park} - v_{earth/jupiter} [/tex]
Is it right, or is it worng?
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:
[tex] v_{\infty} = v_{park} - v_{earth/jupiter} [/tex]
Is it right, or is it worng?