kneejo
Astronut
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sometime ago I planned a trip to Jupiter and put a wheel in orbit around it, but it kept de-orbiting before I arrived there. (about 8 months travel time).
What's a good rule-of-thumb for the altitude of a stable orbit for Jupiter (or any other body)?
My initial thought was that Jupiter's diameter is about 10 times earth, so LJO would be ten times higher.. 300k altitude on earth would have to be 3000k on Jupiter to get the same orbit stability.. but maybe my intuition is wrong about this, and it's not related to the diameter but something else.. please enlighten me on this
What's a good rule-of-thumb for the altitude of a stable orbit for Jupiter (or any other body)?
My initial thought was that Jupiter's diameter is about 10 times earth, so LJO would be ten times higher.. 300k altitude on earth would have to be 3000k on Jupiter to get the same orbit stability.. but maybe my intuition is wrong about this, and it's not related to the diameter but something else.. please enlighten me on this