Comment Re:Recovery != Reuseability (Score 3, Insightful) 108
It's easy to pretend to know stuff. Everyone and their mother nowadays seems to be an expert on rocketry.
It's harder to actually know stuff. The most important causes for failure on rockets are engine failures, software failures, and structural failures, in that order. Engine failures are typically caused by excessive vibration, thermal stress, combustion containment failures (hot gases touching the walls), turbopump failures, and a few other reasons, and these will often show up in static tests. In fact this is the whole point of static testing. As for software, it's the same whether you're re-using an airframe or not. Finally, as for structural failures, they are caused by vibration, thermal stress, and aerodynamic stress. Of these, a pretty good picture can be constructed from static testing, with only aerodynamic stresses left out. Granted, a single-engine test isn't very accurate for diagnosing problems; full-rocket static tests are better.
While flying through the air in a normal mission profile puts a lot of stress on the airframe, it doesn't do any irreversible damage on the airframe, unless the rocket is very badly designed. Going outside the mission profile (facing the wind the wrong way) can and will do irreversible damage, but spacex are very careful to bring their rockets down gently. If you want to bet that a recovered falcon 9 first stage can't be used, the only way that argument will work is if you argue that the airframe somehow suffers irreversible damage during the recovery maneuver. Other than this, it would be extremely strange.