Nope. And NASA themselves is not an aerospace engineering company, they're contracting out the Ares/Orion architecture to other companies, notably ATK for the launcher and LockMart for the capsule.
The problem is that there are multiple issues with the Ares architecture that many people have pointed out. However, until this point, management has failed to address their significance. Former administrator Mike Griffin basically came up with and implemented the architecture himself, anyone that was vocal about problems with it could guarantee they'd be out of their job.
The president created the Augustine commission over the summer to assess the current Program of Record as well as alternatives, and present options, not recommendations, to the president. The committee did acknowledge that Ares is not feasible, and there are better alternatives, however Ares still has the stronghold in the political battle and has the chance of winning out. The committee's final report is to come out tomorrow.
There are a number of alternate architectures that would make much more sense. One is very simple - using EELV's (Evolved Expendable Launch Vehicle) to launch the Orion capsule. It would use the Delta IV Heavy or Atlas V that are currently being used to launch unmanned satellites, with some modifications, to launch the Orion capsule. There would be a number of alternatives for launching cargo, including building the Ares V as planned.
My favorite would be the DIRECT architecture (directlauncher.com), which would take the current shuttle ET and SRB's, essentially attach SSME's (Space Shuttle Main Engines) to the bottom and the capsule to the top. It would require very little in terms of development costs compared to Ares, would retain most of the shuttle workforce (huge political plus), and would use components that have already been tested extensively.
The current favorite among NASA management and the Augustine commission seems to be SD-HLLV "Not-Shuttle-C" which would involve sidemounting the capsule and cargo to a current shuttle stack in place of the orbiter. This carries many of the same advantages as DIRECT, but is less efficient, would require 3 launches instead of 2 for lunar, although scenarios are being considered of using combination SD-HLLV and EELV to launch crew/cargo.
Another option worth mentioning that probably is not likely is Ares V Lite, basically a smaller version of Ares V that would be used to launch both crew and cargo (separate launches). Similar to DIRECT, but it would use the 5 seg RSRM's that aren't currently developed - thus more time and money. But an ET between the SRB's would probably serve as sufficient mitigation for TO.
In somewhat breaking news, NASA Administrator Charlie Bolden has just ordered MSFC to study alternate approaches. This is a very good sign. Hopefully the decision that will be made is the right one.
http://www.nasaspaceflight.com/2009/10/ ... ernatives/