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JayFlynn
- 7
- 0
I am doing research for my aerospace engineering dissertation to plan a mission to a Jupiter trojan asteroid. I was researching the type of outgoing trajectories used in missions such as JUNO, Galileo and Europa and noticed they all use Earth as a gravity assist in getting to deep space. Surely be more efficient and save time if a Mars slingshot was used rather than performing deep space manoeuvres way beyond Mars' orbit just to come back to Earth for a slingshot? Can anyone explain the mechanics of why NASA do it like this?
https://upload.wikimedia.org/wikipe...x-Juno's_interplanetary_trajectory_en.svg.png
https://upload.wikimedia.org/wikipe...x-Juno's_interplanetary_trajectory_en.svg.png