Not quite. You set up a plunging orbit and do a long burn at closest approach. The math/physics give you the biggest change in orbital energy. Slingshot requires no burn and is a three-body interaction.
Not quite. You set up a plunging orbit and do a long burn at closest approach. The math/physics give you the biggest change in orbital energy. Slingshot requires no burn and is a three-body interaction.
Thanks. Sounds like that might have to be their fallback if indeed the main engine is out or fuel is low?
No, they need a working engine and Del V ~ 2.7 km/s to use the Oberth maneuver to leave Jupiter - it's not a fallback, but the heart of what they're proposing.
I meant if they can't do an Oberth
I think the best option is a small burn at Apojove to set up one or multiple flybys at Io/Europa/Ganymede that could then slingshot the spacecraft out to 3I/ATLAS! This could use as little as 200m/s of delta v, maybe even down to 100m/s if done properly, which is much more realistic and doable !
Chaotic orbits are your friend, but that takes patience and time you're not likely to have. And hygiene keeps you from trying close encounters with the icy moons with a dodgy propulsion system. Don't wanna smear Juno all over Europa.
I’m sure theres a trajectory using just Io or Io and Ganymede that’ll work. I’m just not sure how to calculate it! I can do the first Io encounter but after that I’ve just not got the programs
Yup. You want visits from black monoliths? Because that’s how you get visits from black monoliths.