10.1.1 Pressure vessels covered by this Chapter are to be tested on completion to
                                 a pressure, ρT, determined by the following formula, without showing signs of
                                 weakness or defect: 
                              
                              
                              
                              
                              
                              
                              but in no case is to exceed
                              
                              
                              
                              
                              
                                 
                                    where
                                    
                                       | 
                                                 ρ  | 
                                       = | 
                                       design pressure, in MPa | 
                                    
                                    
                                       | 
                                                 ρT
                                              | 
                                       = | 
                                       test pressure, in MPa | 
                                    
                                    
                                       | 
                                                
                                             t
                                              | 
                                       = | 
                                       nominal
                                             thickness of shell as indicated on the plan, in mm | 
                                    
                                    
                                       | 
                                                σT
                                              | 
                                       = | 
                                       allowable
                                             stress at design temperature, in N/mm2
                                              | 
                                    
                                    
                                       | 
                                                σ50
                                              | 
                                       = | 
                                       allowable stress at 50°C, in N/mm2 | 
                                    
                                    
                                       | 
                                                c | 
                                       = | 
                                       corrosion allowance as defined in Pt  5, Ch  11,  1.2 Definition of symbols.  |