Development of Methods and a Program Verification to Determine the Required Volume of Launch-Vehicles And Boosters Flight Testing
A method of determining the required volume of launch-vehicles (LV) and boosters block (BB) (number of starts) flight testing (FT) with a confirmation of their reliability on the basis of these results, experimental testing working-off (ETW), taking into account a possible failure during a flight is proposed. Results of a verification of numerical methods and programs for automated calculations are presented.