[Retracted] A Study of Structural Parameters Effects on Pressure Differential to Roll Titanium Diaphragm for a Spacecraft Propellant Tank

Table 3

Dimensions of the thickness, T and the chamfering radius, R_f for every group.

T (mm)			R f (mm)
Flanging section	Cone section	Arc section
0.40	0.40	0.56–0.60	5, 6, 7
0.60	0.60	0.84–0.90	5, 6, 7
0.80	0.80	1.12–1.20	5, 6, 7
1.00	1.00	1.40–1.50	5, 6, 7