Just Don't Get It
[email protected] is a community for things that you just don't get or understand. It's a community where you're welcome to be the opposite of the smartest in the room. Ask questions about things of which have perplex for years like "why was seeing a pig run a consolation?" or "why don't we shoo our space in to the sun?" and for those of you not comfortable with asking questions, even those like "why is going to bed with your socks on even though you have a spouse a thing?", you're welcome to be part of this community too and answer questions. The only thing I ask is that you be and not a condescending prick.
I originally said "You're free to post text posts, screenshots or memes." but it seems to be mostly text. Feel free to change that with your posts.
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Kerbal Space Program certified astrophysicist here.
Getting into earth orbit is hard enough. Hitting the sun is also surprisingly hard. Well, hitting it is in itself not that hard, but carrying the amount of fuel needed is.
To hit the sun you need to hit an escape trajectory from earth. One you're in low earth orbit, thos isn't THAT hard, but it requires a lot more fuel than one would normally pack into a normal satellite.
And once you've escaped earth, that's where the real fuel expenditure has to happen: do nothing, and you'll remain roughly coplanar with earth (and in all likelihood eventually be recaptured by earth gravity). What you need to do is to burn retrograde, as in slow down your orbit, so you start falling straight towards the sun instead.
Wait, I've just met my first celebrity on Lemmy. I need to keep this moment stored in my memory banks.
Okay, my first question isn't the space debris all in earth's low orbit already?
Second question, can't you ride the orbit and then use a tiny thruster to leave the atmosphere and follow that trajectory straight towards the sun. I imagine the calculations needs to miss every planet between us and the sun wouldn't be simple, but thirdly, technically this should be possible right?
Think of it as a representation of how much energy is needed for orbits. To get to the moon you need about 1.7 km/s of delta v. To get to sun you need 30 km/s of delta v. To escape our solar system you only need 18 km/s of delta v.
Think of it this way. The earth is moving horizontally to the sun at 29.78 km/s (107,200 km/hr). In order to hit the sun you have to cancel all of that movement otherwise You'll miss the sun and enter a new elliptical orbit.
Hmmm, I was thinking we could slingshot our own orbit. Use the centrifugal fly South and use a couple thrusts to point towards the sun. I was clearly over simplifying it.