4 ms·
Seems unlikely. One is slamming due to a heavy glideslope. Two is slamming due to a serious yank on the rear section. The airframe stresses and flight dynamics
by bronson 3y ago
Seems unlikely. One is slamming due to a heavy glideslope. Two is slamming due to a serious yank on the rear section. The airframe stresses and flight dynamics will be different.
- euler_angles 3y agoYeah, dynamics will be different, though caveat I am not a structures/loads engineer. I just don’t think anyone had the risk appetite to chance a test asset against a very difficult to achieve test point.
- hef19898 3y agoIt is also fair to assume the decision to not do additional testing of wire-only arrests was well analyzed by the respective engineering teams. Program management does not take decisions like this by themselves.
- euler_angles 3y agoAbsolutely. We had a whole carrier suitability team full of people who lived and breathed this stuff. It was just my responsibility to make sure the aircraft instrumentation system got them the data they needed, at a high enough quality, to empower their analyses and decision making process.