Study on the Failure of the Bolted Flange Connection Structure between Stages of Missiles (Rockets) under Transverse Impact Load

Figure 8

The failure process in the experiments. (a) 0 ms, (b) 5 ms, (c) 10 ms, (d) 15 ms, (e) 20 ms, and (f) 25 ms.

(a)

(b)

(c)

(d)

(e)

(f)