Design of the Space Camera Protection System during Launch Process

Table 6

Identification load of the three direction sinusoidal vibration screws (from Supplementary Table 1–3).

Direction	F1 (N)	F2F3 (N)	M1M2 (N·M)	M3 (N·M)
	226.9	43.9	116.2	32.1
	221.0	39.2	110.0	26.8
	214.1	74.7	291.2	40.8