Given that this test, while useful, didn't actually use any of the components of a man-rated Ares I, I'm not that excited.
Ares I will use a new 5 segment Solid Rocket Booster (SRB), this was the good old STS 4 segment SRB.
Ares I will use the J2-x powered upper stage, this was a weight equivalent mock-up.
Ares I will use the Orion capsule and it's engine to finish up the orbit, again, just a mock-up with right szie and weight.
Ares I flight control software not built yet, but that's ok, as the hardware it will guide wasn't here either.
You know when the car companies build a clay mock up of that new model? That's about where this Ares I-x test was. Baby steps are ok, but I was hoping for more return on investment.
So I'm annoyed that the test program hasn't progressed further, but in reality, this is rocket science, and at least they got the thing off the ground in a reasonable fashion. The problems here go a lot further than my unease that NCSA isn't that far along for the time and money they've already spent. Here's a list of issues that they still have to face in making this a viable launch system:
What's the lifting capacity of the ARES I? 25mt? That was the declared goal. 24 mt? That was a compromise when other issues crept in. 20 mt? Where the current design is, but Ares I needs 25 mt of lift for an Orion capsule with safety features and lunar capability for 4 crew, and doesn't have it.
Also, when is the Ares I scheduled to fly with the Orion capsule, even in a non-man-rated test? 2013, as NCSA originally planned? 2016 as the Augustine commission recently claimed?? Before the Space shuttle stops flying? Before the ISS is de-orbited? Be nice for NCSA to have a way to get our astronauts to the ISS without "borrowing a Soyuz."
More importantly, how much has NCSA spent on the development of the Ares I to date? 5 billion? 6 billion? They still have to finish the 5 segment SRB design and tests, the J-2x Upper stage engine and tests, the new upper stage and tests and the Orion capsule and tests before any manned flights can take place. That's got to be another $5 billion easy. All this to get the lift capacity of an Atlas V or a Delta IV heavy and a theoretical better safety rating.
Lastly, one reason the Ares I was chosen was that it was supposed to be safer for the crew than any alternative. But there's this- http://www.newscientist.com/blogs/shortsharpscience/2009/07/death-knell-for-nasas-ares-roc.html. I feel sorry for the hard-working engineers at NCSA, and I hope that the new management can get them back on track with a better design.