Riding an Ion Drive to the Asteroid Belt

Iron Condor writes "JPL is now close to embarking on another of its trademark, one-of-a-kind missions, this time to the heart of the asteroid belt: The Dawn mission is being prepared for launch this summer from Kennedy Space Center. Dawn will explore Ceres and Vesta, the two largest known asteroids in our solar system, which lie in the vast expanse between Mars and Jupiter. In the process, the mission will make history on several fronts. Besides being the first spacecraft to orbit a main-belt asteroid and the first to ever orbit two targets after leaving Earth, Dawn will be the first science mission powered by electric ion propulsion, the world's most advanced and efficient space propulsion technology."

Comments

Not the first ion thruster propelled spacecraft

[thue]

From the summary: Dawn will be the first science mission powered by electric ion propulsion

No, a quick Wikipedia check says otherwise: http://en.wikipedia.org/wiki/Ion_thruster#Missions . For example, Deep Space 1 used electric ion thrusters.

Re:Not the first ion thruster propelled spacecraft

[lobotomir]

Japanese and European science/tech validation space missions have also used ion propulsion.

Re:Not the first ion thruster propelled spacecraft

[TheRaven64]

I believe you could make a distinction between science and technology missions. To my knowledge, all previous missions involving ion propulsion have been for the purpose of testing ion drives, while this one is expected to perform scientific exploration and happens to use an ion drive.

Re:"Electric ions"?

[cnettel]

The propulsion is electric, as in the energy source being electricity, although some mass is still needed for the actual thrust, hence the ions.

Re:Two targets?

[Anonymous Coward]

It's not difficult to do if the two objects are in approximately the same orbital path. So, perhaps, we might soon get a probe looking at Phobos and Deimos.

Of course, most probes orbit the Earth for a while after launch, before injection into their transit path. All the early moon probes orbited both the earth and the moon, and the manned ones then orbited the earth again after return. So you could say that three targets have been orbited before, back in the '60s. This was just the project team looking for a 'first' to impress Americans with.

I suppose the difficulty levels go:

Orbit your base
Orbit your base and your target
Orbit your base, then gravity assist from other object, then orbit your target
Orbit your base, then gravity assist, then swing by one target, then orbit final target (typical multi-planet probe)
Orbit your base, then gravity assist, then orbit one target, then orbit another.

In fact, I was most impressed with the few probes which altered their trajectories in mid-mission to do swing-bys of targets of opportunity. You need flexible fuel provision to do that!

Correction

[FrostedWheat]

Dawn will explore Ceres and Vesta, the two largest known asteroids in our solar system

Correction: Ceres is now the smallest dwarf planet.

Re:"Electric ions"?

[ArieKremen]

The European Space Agency (ESA) has recently sent a satellite to the moon using ion propulsion. (http://www.esa.int/SPECIALS/SMART-1/SEMLZ36LARE_0 .html)

Re:"Electric ions"?

[Rei]

The Isp (specific impulse) on ion drives varies considerably depending on the type of drive and its operational situation. Chemical rockets are typically 300-450 sec. Ion drives (depending on how broadly you accept the term "ion drive") usually range from 1,000 to 20,000 sec. Of course, Isp isn't the only factor to consider -- you also need to consider thrust, mass (including voltage regulation hardware), and efficiency.

There are some really neat drives on the horizon that combine the best of thermal and ion drives, such as VASIMR. The particles are heated with radio waves to extreme temperatures (like in some fusion apparatuses), but since they're ionized, they're affected by magnetic fields. The fields collaminate them into a spiralling plasma, converting their chaotic energy distribution into a directed flow. A magnetic nozzle then redirects this out the back. Moderate thrust plus high ISP -- a nice combination.

My favorite "long range" design is the dusty fission fragment rocket. Most of the energy of fission reactions is contained in "fission fragments" -- basically, the fission of your fissionable fuel blasts microscopic fragments of the fuel at high speeds. In a normal reactor, these bump into the rest of the fuel or the moderator and are "thermalized"; the heat is then converted into electricity lossily. In a fission fragment reactor, the design is such that the fragments (where are inherently ionized) are allowed to escape the core; they can then be A) decelerated to produce electricity, or B) redirected with a magnetic field and vented out the back to produce a ridiculously high ISP thrust. You can do that with ionized particles. :) The "dusty" part comes from the reactor design. The fuel is nanoscale particles of enriched uranium mixed with graphite. Fission reactions automatically ionize the particles, so to keep them suspended at an even distance from each other, all you have to do is ionize the walls of the reactor. Since the particles are so small, their surface area to volume ratio is incredibly large, making radiative cooling realistic. The radiated heat itself can be turned into extra electricity (and even a bit of extra thrust)