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Ion Drive Restarted
Palomar
post Aug 27 2005, 12:44 PM
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After 5-month hiatus

*...the ion drive has been "nominally" restarted.

QUOTE
The EP power is being set to 1325W due to the Sun distance seasonal effect.


QUOTE
The EP operations are planned to last until mid September assuming simulator behaviour. The second half of September has been reserved for possible special operations in case the engine does not behave as expected.


Also lists future activities and gives a rundown on status. All is well, it seems. Includes photo of the ion drive and its "exhaust."
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abalone
post Aug 27 2005, 12:52 PM
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QUOTE (Palomar @ Aug 27 2005, 11:44 PM)
After 5-month hiatus

*...the ion drive has been "nominally" restarted. 

*

It was described once in an article the I read somewhere as being equal to a "mouse's fart" in thrust, does anyone know how they keep the mouse alive and farting for so long?
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Bob Shaw
post Aug 27 2005, 01:01 PM
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QUOTE (abalone @ Aug 27 2005, 01:52 PM)
It was described once in an article the I read somewhere as being equal to a "mouses fart" in power, does anyone know how they keep the mouse alive and farting for so long?
*


Is that a PS/2 mouse or a USB one?


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abalone
post Aug 27 2005, 01:05 PM
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QUOTE (Bob Shaw @ Aug 28 2005, 12:01 AM)
Is that a PS/2 mouse or a USB one?
*


Do they have a different thrust to mass ratio?
I think it would have to be cordless
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Phil Stooke
post Aug 27 2005, 05:00 PM
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They feed it lentils?

Phil


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Also to be found posting similar content on https://mastodon.social/@PhilStooke
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ljk4-1
post Jan 16 2006, 05:49 PM
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The European Space Agency and the Australian National University have successfully tested a new design of spacecraft ion engine that dramatically improves performance over present thrusters and marks a major step forward in space propulsion capability.

http://www.physorg.com/news9786.html

The new engine is over ten times more fuel efficient than the one used on SMART-1.

"Using a similar amount of propellant as SMART-1, with the right power supply, a future spacecraft using our new engine design wouldn't just reach the Moon, it would be able to leave the Solar System entirely," says Dr Roger Walker of ESA's Advanced Concepts Team, Research Fellow in Advanced Propulsion and Technical Manager of the project.


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I see that such intercourse long continued would make one thoroughly prosaic, hard,
and coarse. But the longest intercourse with Nature, though in her rudest moods, does
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no sympathy, I go to commune with the rocks, whose hearts are comparatively soft."

- Henry David Thoreau, November 15, 1853

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Toma B
post Jan 16 2006, 05:55 PM
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Amazing!!! Well done!!! smile.gif smile.gif smile.gif
QUOTE
The test model achieved voltage differences as high as 30kV and produced an ion exhaust plume that travelled at 210,000 m/s, over four times faster than state-of-the-art ion engine designs achieve.
This makes it four times more fuel efficient, and also enables an engine design which is many times more compact than present thrusters, allowing the design to be scaled up in size to operate at high power and thrust.
Due to the very high acceleration, the ion exhaust plume was very narrow, diverging by only 3 degrees, which is five times narrower than present systems.
This reduces the fuel needed to correct the orientation of spacecraft from small uncertainties in the thrust direction.


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My "Astrophotos" gallery on flickr...
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