Ion-Engine Spacecraft On Moon Mission
anactofgod writes "The Times On-line and space.com reports that the European Space Agencies Smart-1 probe has cleared the Lagrangian point between the Earth and its moon and is due to enter lunar orbit on Nov 15th. Smart-1's mission is to make observations related to the moon's formation and composition.
What's cool about this mission, other than this is the first European mission to Earth's moon, is that the probe is using solar powered ion engine thrusters. Ion engines are an order of magnitude more efficient than chemical engines. NASA flew the first ion-powered spacecraft, Deep Space 1, in 1998. Smart-1 is the second spacecraft to use the technology, and was designed as a testbed for future ESA missions. The ESA is scheduled to fly the ion-powered BepiColombo on a mission to Mercury in 2009."
The lagrange point is where the gravity from the moon offsets the gravity from the earth, making a point where there is no gravitational pull towards either body.
- Zav - Imagine a Beowulf cluster of insensitive clods...
The lagrange point is where the gravity from the moon offsets the gravity from the earth, making a point where there is no gravitational pull towards either body.
Not quite -- it also includes the "centrifugal" pseudoforce. The Lagrangian points are fixed points within the rotating reference frame of the Earth/Moon system. Because the frame rotates, it is not an inertial frame, so pseudoforces contribute. If the Earth and Moon were held in place magically, instead of orbiting each other, the balance point between us would be in a different location than it is when the system rotates.
Also, of course, there are five Lagrangian points, only one of which is physically between the Earth and Moon. If only gravity mattered, it would be the only one. The other four arise thanks to the contribution of pseudoforces.
I heard recently about a new Nuclear Thermal design (in http://www.wired.com/). I'm wondering if this is better (higher ISP per unit cost) than an Ion thruster.
Obviously, if you're headed inbound into the solar system, you're destined for more light therefore more available energy. And, going outbound (Pluto-wise), sunlight gets scarce. So, where is the breakeven? Solar panels cost weight, and Ion engines mass a lot for the miniscule thrust they generate. Nuclear thermal (or Nuclear/Ion) combinations also mass a lot but have the added advantage of much higher available thrusts for short bursts if needed.
What about pairing Nuclear thermal with Ion thrusting? Generate a plasma by heating it with a slow fission or plutonium decay reaction, and also generate electricity from the waste heat. Use the electric power to do microwave heating. Or, directly accelerate the plasma ions using a magneto-hydrodynamic MHD setup?
Is anyone actually actively developing anything like this? It seems to me that the fundamental limitations of our current space delivery systems are NOT who can build a better mousetrap, but that all the mousetraps are using cheese (LH2+LOX) instead of peanut butter (NTR, MHD, Ion engines, etc.).
Also, are there any somewhat-better-than-rumors of USAF designs using these that are flying but that people can't talk about?
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A nifty diagram is available here.
As I seem to recall, there are a group of asteroids in the L4 and L5 points (with regards to the Sun and Jupiter) called the Trojan Asteroids. Not shure that this is relevent, but the factoid just popped into my head.
In terms of number and diversity of missions, the ESA actually seems to be a lot more active than NASA overall. (That might just be perception, who knows.)
Does anyone have any info on the relative activities/funding of NASA vs ESA?
It's super cool that they're experimenting with newer propulsions sytems and the like.
Lost at C:>. Found at C.
You can see a picture of the Trojan asteroids here. Jupiter is on the left of the page and revolves counter-clockwise. The trailing Trojans at L5 are 60 degrees behind Jupiter, near the top of the picture and the leading Trojans are, of course, 60 degrees ahead, near the bottom of the page. There are also a smattering of bodies around the L3 point. The Solar-Jovian L3 is closer to Jupiter's orbit than the diagram in the parent post would indicate.
Sometimes, the L4 and L5 Lagrange points of a system are called Trojan points.
This site mentions how the prominent asteroids at the Trojan points are named after characters from the Iliad. One group is named after Greeks, the other after Trojans. Each group also has a "spy" in its midst.
Don't blame me, I voted for Durga.
I don't have an answer for you, but I think that the idea of powering a ion thruster with nuclear material is an interesting one. The question is whether the mass required to generate power for a reasonable amount of time is more than the mass of solar panels to power it for a similar amount of time.
It seems like such a logical design change that I am sure it has been considered. It would totally kill the level of complexity though, which may be enough to kick it out of practicality regardless.
Cool stuff in general though. The idea of low levels of constant acceleration is very attractive for long distance probes. Not necessarily fast enough for manned missions though.
Cuchullain
"If sharing a thing in no way diminishes it, it is not rightly owned if it is not shared." -St. Augustine
I looked on wikipedia, but was turned off because of the spartan nature of the article.
Not "spartan." "Trojan."
Don't blame me, I voted for Durga.
Smart-86, which will almost get to its destination but will wind up saying "Missed it by that much!"
Sustainability and energy independence essay
Why newspapers publish drivel like this, I'll never know. If it was hard to get right you wouldn't have amateurs fisking this stuff on Slashdot!
Sustainability and energy independence essay
So, what, it's got an engine from General Motors' latest economy car? If so, I hope it goes on a mission to the ringed planet next.
This is a recent article from earlier in the week about this mission.
This thing took a year to get to the Moon. Yes, it's a testbed for ion propulsion, but if it takes a year to get to the Moon, ion engines aren't going to help us much.
We need propulsion technology that moves bigger things faster, not smaller things slower.
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Here's a picture of the ion craft that went to the moon.
It is easier to build strong children than to repair broken men. -Frederick Douglass
That was no moon, it was a space station.
It is easier to build strong children than to repair broken men. -Frederick Douglass
Such crafts would not need to orbit the sun and you could put them almost anywhere. In fact, you could launch them in almost any direction within the solar system and establish the equilibrium between solar wind and gravity.
And why not provide them with an ion engine? Imagine if the sun went out, the things would simply plummet to their doom otherwise and all the hard work would have been for nothing.