Design-Engineering Principles of Standardization of Characteristics of Solid-Metal High-Pressure Tanks in Rocket and Space Machine Building

Based on analysis of literary sources it was discovered that solid-metal high-pressure tanks were unique object. It allows dealing with an actual problem of rocket-and-space machine building which is the standardization of rocket-and-space machinery. It was suggested to use internal energy accumulated in pressurized gas as an object of statistical analysis. This internal energy specifies running efficiency of high-pressure tanks within rocket-and-space machinery. Algorithms of optimization of design characteristics of high-pressure tank by the criterion of weight and prime cost were worked out. The algorithms take special features of tank production (dependency of defectiveness of joint weld and thickness of wall of spherical tank, the influence of hemisphere production method on weight of the tank, production expenses, etc.) into account. The algorithms allow optimization of design characteristics of high-pressure tanks which operate under cryogenic temperatures. Shown that thanks to the significant contribution of cost of stainless steels and titanic alloys in prime cost of all-metal HPB results of optimization of parameters of balloons on criteria of weight and prime cost coincide.

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