Thanks Chris. I appreciate your comments. I believe I meant that at 2500', I can observe everything from the ground, I can see how the chute(s) deploy, the ejection charges at work, etc. With these observations, I can then predict how it will perform at higher altitudes. I do not expect to see it at 8000' or at 17,000'. I will be relying on the trackers. I should see the deployment at 1000', where the primary altimeter is programmed to deploy the main, and at 750', when the back-up fires, then I should certainly hear and see the deployment. To see it at 2500' is the reason I would test fly before the certification flight takes place. It is not a break in flight, it is a test flight. Unless you have something really unusual, you do not need to break anything in. That takes place on diesels and other internal combustion engines (ICE) where you have bearings, rings, valves, etc, that need a moderated and stepped break in period. Or at least that is the way it used to be, but say on helicopter turbines, we had a dyno test stand for testing for pressures, leakage around seal, and look for any other issues before it was placed back on the helicopter. It was brief though, because those engines only had a certain number of hours life span before it was rebuilt, so it was tested to see if it worked, then shut down and those minutes or hours were added to the log. That is not necessary on a rocket. I hope I am making sense here. BEAR