I don't think anyone will be leaving that atmosphere with chemical propulsion any time soon...
I don't think anyone will be leaving that atmosphere with chemical propulsion any time soon...
Gravity on surface of this planet will be 3(times heavier than earth)/(1.55(radius)^2), so 1.25g, however escape velocity also depends on planet radius so we get sqrt(1.55 * 1.25) = 1.4 earths escape velocity (so 15.7km/s). Assuming Isp specific impulse of engine of around 300s, let's compute m0/mf (initial mass of rocket / payload) = exp(vEsc/(Isp*g0)) (g0=9.8m/s^2 (on both planets)):
For earth, it's 45.
For this planet, it's 208.
So, the rocket (using our current chemical engine technology) needs 4.6 times more fuel than on earth. Much more difficult, but maybe possible...
edit: formatting
Plus, if it would take something like a Saturn V just to put the mass of a potato into low orbit I could easily envision an extraterrestrial civilization thinking it wasn’t worth the cost to try.
I'm sure that's true holding all else the same, but all else isn't the same.
Maybe it's airless due to stronger stellar winds.
That's why it doesn't really help much to launch rockets from a balloon -- getting there is not a problem.
TOI-715 b has a log g value of 5.0 +/- 0.2. Earth is 2.992.
>>>ts mass is 3.02 Earths, it takes 19.3 days to complete one orbit of its star, and is 0.083 AU from its star. Its discovery was announced in 2023
https://i.imgur.com/ghLnFrH.png
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What would gravity be on that thing, it doesnt say what its circadian rhythm is.. so how long is a day, if a "year" is 19 earth days (or is the period in 'day' local-solar-system-days?)
It'd be pretty messy to instead define things in the database in object relative terms, particularly when you usually know things like the orbital period with significantly more accuracy than rotational velocity.
Thanks, though - I wasn’t sure if we always use a local reference but then au is as local a unit as possible at these scales.