Using the math from "Rocket Propulsion Elements" [2] it seems like for anything other than a needle shaped projectile it would not be practical.
[1] http://www.navytimes.com/news/2008/01/navy_railgun_test_0801...
[2] http://www.amazon.com/Rocket-Propulsion-Elements-George-Sutt... Pretty much everything there is to know about rockets that isn't classified.
The book "Rocket Propulsion Elements" [1] which is pretty much everything known about rockets that isn't classified, is pretty dense for a reason. I certainly don't hold it against the journalists who are trying to do their job as best they can.
That said, because launching heavy things into space can also be used to launch heavy things around the globe and into other peoples territory, there are aspects of the technology that are closely watched. One of them is cryogenic turbo pumps. These are pumps which can pump a cryogenic fluid at high pressure and flow rates. Those are an essential part of the space puzzle because once you get a functional cryogenic rocket engine you can add additional engines and fuel at a relatively constant mass/payload ratio. And then that means if you have a payload of mass X, and an orbit of O (or sub-orbit if you're talking ICBM) you can build a delivery system to make that work. Of course other controlled technologies are guidance systems and launch 'racks'.
If Iran was looking for something more than a PR ploy I think they should host a middle east space conference with peer reviewed papers. To get to where SpaceX is, and where Iran wants to be, is rocket science but it is also achievable rocket development. Open discussion would lend an air of legitimacy to the research (today most westerners assume its simply a quest for missile technology) and probably advance their programs more effectively.
[1] http://www.amazon.com/Rocket-Propulsion-Elements-George-Sutt...