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Saw this quote in the WSJ[1]: > Alan Fitzsimmons, a DART investigation team member and astronomy professor at Queen’s University Belfast, said he would like th
by skue 4y ago
Saw this quote in the WSJ[1]:
> Alan Fitzsimmons, a DART investigation team member and astronomy professor at Queen’s University Belfast, said he would like the gravity tractor technique tested next, “because it’s actually very difficult to accurately guide and maneuver spacecraft in very close proximity to an asteroid.”
For the gravity tractor technique, I’m curious whether any experts here could explain just how challenging it would be to have a spacecraft match the speed and path of an asteroid headed to Earth. Could you take an elliptical path, and how much fuel would you need to match the asteroid’s velocity? How would that compare with past missions with a return component (e.g. the moon)?
As a layperson, just smashing into an asteroid seems like much simpler technique, if admittedly less elegant.
[1] https://archive.ph/20221011184904/https://www.wsj.com/articles/nasas-asteroid-smashing-dart-mission-deemed-a-success-11665512765 https://archive.ph/20221011184904/https://www.wsj.com/articl...
- mlindner 4y agoThe thing with the gravity tractor is that all the energy needs to come from the spacecraft itself. Whereas with impactor design you can use energy from the Earth's relative motion to the incoming object.