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SpaceX F9 - DART - SLC-4E

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2nd stage need not return, having pushed to escape velocity. Space is big, it’s not coming back. Likely in an eccentric solar orbit now, either eventually burn up or not meet another body for a very long time.
Isn't the satellite (payload) and the 2nd stage in the same orbit, with the 2nd stage pretty much following the satellite? Until such time the satellite fires off its own rocket engine for any course correction.
 
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Isn't the satellite (payload) and the 2nd stage in the same orbit, with the 2nd stage pretty much following the satellite? Until such time the satellite fires off its own rocket engine for any course correction.
Yes. The satellite does have its own engine and will still be accelerating and maneuvering. Someone who likely knows said the second stage is in a heliocentric orbit. So little need to do anything about it. It's the stuff in LEO to MEO that needs to get cleared out.
 
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someone more informed about such things pointed out that a kick stage would add more mass that could instead be used as fuel

FWIW from a pure mass efficiency perspective, staging is almost always the better solution; It would be far more efficient for the "last bit" of the launch stack to not carry around 4T of F9 second stage.

Where reality steps in is with things like cost and complexity and launcher capacity. Cost probably wasn't a huge factor in this one, but certainly a dedicated kick stage costs more than "more propellant" on an existing stage. (Note that DART's prop system is electric and so is impractical for para/hyperbolic orbits). Complexity more of less boils down to the fact that every additional, thing that has to go right is one more thing to go wrong. But...what is most likely in this scenario is that F9 simply had enough additional capacity that it could serve this mission without an additional prop system.
It's the stuff in LEO to MEO that needs to get cleared out.

Yep, and practically speaking, its really only the stuff in low LEO. That's starting to change and include high LEO, but anything beyond (including MEO)...those stages aren't coming back for a while...
 
I was wondering if they could have sent two probes - joined together - separating at around 1 minute mark, with the first one firing a small thruster and crashes ahead, and the 2nd one captures the video of that crash
Turns out they had another camera in space - possibly much closer than ground telescopes - watching the collision. Atleast that is how I understood this.


Fifteen days before impact, DART’s CubeSat companion Light Italian CubeSat for Imaging of Asteroids (LICIACube), provided by the Italian Space Agency, deployed from the spacecraft to capture images of DART’s impact and of the asteroid’s resulting cloud of ejected matter. In tandem with the images returned by DRACO, LICIACube’s images are intended to provide a view of the collision’s effects to help researchers better characterize the effectiveness of kinetic impact in deflecting an asteroid. Because LICIACube doesn’t carry a large antenna, images will be downlinked to Earth one by one in the coming weeks.


It was just amazing they were able to get live video from an object around 50 light seconds away.
 
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Scott Manley mentions the orbital period of the moonlet is approx. 12 hours. Do we know how far is the moonlet from the parent body?

Based on the video, I recon it took 90 seconds after passing the parent body and impact. Given that the satellite was travelling at 14,000 miles per hour, the distance between them is perhaps 350 miles or less. A distance where you cannot see the moonlet from the parent body through naked eye. Or maybe just as a small dot.

Also do we know if this was a head on collision or rear end? For sure it is almost impossible to do a side hit.

What speed was the asteroid travelling?
 
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What speed was the asteroid travelling?
Google “orbital velocity of asteroid belt”. I found an online reference for you:
The average orbital speed of a main-belt asteroid is 17.9 km/s, the orbital speed of Ceres. Ceres has a pretty typical orbit and makes up a third of the Belt by mass.
Asteroids that have significantly eccentric orbits move faster that their average when they are near their perihelion and slower than their average when they are near their aphelion, in accordance with Kepler’s Second Law of planetary motion.

Asteroids whose orbit has a semi-major axis longer than Ceres’ have average speed slower than Ceres’ average speed, and asteroids whose orbit has a semi-major axis shorter than Ceres’ have average speed faster than Ceres’ average speed, in accordance with Kepler’s third law of planetary motion.