The big difference between these engines and the normal type of ion engine is the specific impulse of the engines. For memory, the SI of these engines is an order of magnitude or more larger than normal engines. Plus they also have a greater exhaust velocity than normal ion engines and can also operate at higher voltages. The VASIMR engine has been operating at 200kW and a thrust of 9 Newtons which is a lot more than normal engines can handle. The thrust is still low, however, it's larger than present systems.
In order to get to Mars in a month or so, they'll need engines that can run at 20-30MW, which is possible. The present power output is more than adequate for Earth orbit and Earth-Moon usage.
Here's the
HDLT and
DS4G, both Australian engines.
Here's some news on the systems...
http://www.azom.com/news.asp?newsID=4751
http://www.esa.int/esaCP/SEMOSTG23IE_index_0.html