New Engine Raises Possibility of Cheap Travel To the Moon
shreshtha writes with this intriguing bit from The Daily Mail: "A tiny satellite thruster which can journey to the Moon on just a tenth of a litre of fuel could usher in a new low-cost space age, its creators hope. The mini-motor weights just a few hundred grams and runs on an ionic chemical compound, using electricity to expel ions and generate thrust. The tiny motor isn't built to blast satellites into orbit — instead, it's to help spacecraft manouevre once they're in space, which previously required bulky, expensive engines."
To whom shall I write the check as I securely invest my life savings?
Strange things are afoot at the Circle-K.
I was under the impression that fuel to get to the moon isn't a major issue, if you can launch a few years before you need to be there. There's (almost) no friction to stop you...
You do not have a moral or legal right to do absolutely anything you want.
Seriously, I can travel to the Moon with no fuel if I start in the right position with the right momentum. TFA doesn't tell us much unless the secrets are hidden in the video I'm blocking on the bottom of the page.
"I zero-index my hamsters" - Willtor (147206)
Who would have guessed this got posted by Timothy!
Slashdot: providing anti-social weirdos a soapbox, since 1997.
If this were news for nerds, maybe someone would have researched this before posting?
Forget it, Jake. It's Slashdot.
Dog is my co-pilot.
The new thruster has nothing to do with getting to the moon or even getting into space. It's a way for a small satellite to maneuver once it is in orbit. It could possibly be used for getting into lunar orbit from low earth orbit, but its intended purpose right now is to help clean up debris.
http://www.projectrho.com/rocket/enginelist.php#id--Ion
It's a great site which details (with lots of math) the various problems with space travel.
is launching to space from earth/moon surface. Traveling once there, and landing (at least in earth) could be relatively inexpensive. But once the space elevator, space fountain or other approaches are built and gives us relatively cheap ways to reach space, this kind of approachs could make a difference.
Well over a decade.
The fundamental problem with ion thrusters (as a general class) is that you trade power use for fuel use.
Yes, they may use lots less fuel.
http://en.wikipedia.org/wiki/Specific_impulse#Examples - for example.
An advanced ion thruster may use nearly 1/50th of the fuel of a conventional rocket engine.
But, it needs 50 times the power to do this.
So, to replace a conventional rocket engine burning a kilo of fuel a second, and producing a thrust of perhaps 500kg, with no electrical requirements, you need about 20 grams of fuel a second, and around 450 megawatts of power.
Needless to say - for many applications, the power plant ends up heavier than the engine it's replacing.
It only works in very low thrust applications.
The low thrust also brings other problems.
For example, around the earth is a belt of charged particles.
Ascending through these on conventional rockets is not a problem. You do it so rapidly.
With ion engines, you need to slowly spiral out (due to being power limited), and your whole craft gets highly irradiated.
This ion thruster is unique by its extremely small size. we have miniaturized not only the ion emitter, but the entire thruster including high-voltage electronics and tank. Our complete thruster has a mass of 200g (including 100 ml of fuel), thus allowing it to be used on nanosatellites. It is the first high efficiency electric propulsion system that can be used in cubesats and 5kg satellites, such as those being planned for OLFAR The principle of operation of colloid thruster a bit different from the ion engines used fro instance on SMART-1, which uses ionize Xenon. in our case, we use a particular conductive liquid, an ionic liquid, from which we can extract both positive and negative ions. using a liquid avoids a pressurized tank, and allows for important simplification of the system (no valves, no heavy tanks, all flow controlled by capillary and electrostatic forces. using the ionic liquid allows the same speed as using a gas, but offers one big advantage: since we emit (from 2 chips in parallel) both positive and negative ions, the spacecraft stays electrically neutral, which is essential for electric propulsion to avoid having the ions fly back to the spacecraft. for more conventional electric propulsion systems, only positive ions can be emitted, so a neutralizer is needed to emit electrons to keep the spacecraft charge neutral. not having a neutralizer allows significant mass and power savings.
I'm biased, 'cause I work on this!
http://lmts.epfl.ch/microthust
- Herb Shea
and that is not the big issue, as getting off the ground is always the big expense, but we all know that. This tech can be useful in reducing weight costs for sub orbital payloads though, and probably resembles the design of a DS4G engine. The problem with efficiency in the past is that motors required high voltages to accelerate the ions that collided with the electric field grids. DS4G used a two stage four line grid with the top grid closely spaced and of higher voltage, with an open spaced lower voltage bottom grid. These differences between these stages allow higher velocity without ion grid collision at overall lower voltages resulting in 4x the fuel efficiency of previous engines.
Well - yes, and no.
The fundamental problem with microwaves is - they're microwaves. ... - they undergo diffraction.
They are just another sort of radio, and like all radio waves, and light, and
This limits how much you can focus them.
A 'small' transmitter antenna of say 1km, with microwaves of about 10cm wavelength, will have a beamwidth of about:
1.22*.1m / 1000m.
This is a beam which spreads about one part in ten thousand.
After 10000km, the beam will be one kilometer in diameter. At the distance of the moon - 40km.
So, you need an antenna 4km in diameter on your craft simply to pick up one percent of the beam at the moon.
Range is a major problem.
Lasers work somewhat better - but have their own annoying issues.
Parent link is bad. Try this:
http://lmts.epfl.ch/microthrust
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