Breaking news: The thing we put in a highly elliptical orbit around the sun is in a highly elliptical orbit around the sun (and hasn't yet reached its perihelion).
I'm theory, the previous record holder is actually a particular man hole cover involved in operation plumbbum. Some napkin math put it at somewhere around 37 miles per second. A high speed camera pointed at it only caught one or two frames of moment.
It's too bad they can't fling the probe in the opposite direction once it's done with the sun. I know it's instruments are probably tuned specifically to take measurements of various solar phenomenon from close-up and probably aren't sensitive enough to be useful for any deep space science, but it'd be cool to use that speed to launch it on an escape trajectory and see how long it takes to catch up to the Voyager probes.
Thanks for the math! Here's hoping we can fling the records of our civilisation far enough out for another civilisation to learn about our demise. And not, like, just accidentally flinging it into a burning star or space imperialist Klingons or something. Even though that would be poetically appropriate too.
It's only going that fast because it's near the sun. The same way a satellite close to Earth needs to move faster than one farther away. You can't really use that velocity to go elsewhere. It had to lose a lot of energy to get as close to the sun as it is. It would need to gain that back to get to earth.
I'm really blanking on a way to explain this concisely and I can't explain orbital mechanics in a Lemmy post.
If you play Kerbal space program, you can definitely use that to get a very intuitive understanding of this concept.
Drop a ball. It goes fastest just before and after it hits the ground, and slows down until it gets back to near the height you dropped it from
The probe is the ball, and slingshotting around the sun is like bouncing off the ground. The potential energy (height of ball/distance from sun) gets converted to and from kinetic energy (speed).
Thanks! I didn't think about the fact that it'd lose velocity to gravity as it gets further away.
I wonder if you could slingshot a probe by firing it to fly by the sun and then shedding mass at its perihelion. The idea being that the craft would be mostly dead weight, increasing the force exerted on the craft by the sun's gravitational pull. Once you reach the perihelion, you eject the mass behind the craft so that there's less force acting on the craft as it moves away from the sun.
The Parker Solar Probe is currently traveling at 635266 kph. Voyager 1 travels at 60977 kph relative to the sun and was launched 46 years ago.
So the Parker Solar Probe is ten times faster than Voyager and would pass it in, give or take, five years.
Well yeah, that's how orbits work. You accelerate down to your periapse, the closest point to the body you're orbiting, then slow down on the way up to your apoapse, the furthest point. Thus the probe will keep accelerating until it gets to its closest point to the sun.
It's only going that fast because it's near the sun. The same way a satellite close to Earth needs to move faster than one farther away. You can't really use that velocity to go elsewhere. It had to lose a lot of energy to get as close to the sun as it is. It would need to gain that back to get to earth.
I'm really blanking on a way to explain this concisely and I can't explain orbital mechanics in a Lemmy post.