Improving the Mass Perfection of Composite Cylindrical Shells of Rocket Fuel Tanks

Nowadays, computing capabilities are gaining high performance. Software development has a very positive impact on the СAE of a system. A modern engineer always has tools in his arsenal that allow him not only to design but also to calculate a structure. Predict where the potential destruction will be, etc. Improving the mass sophistication of fuel tanks in rocket and space technology (RST) is an important task to ensure the safety and reliability of space missions. Fuel tanks are critical components of rocket and space technology, as they provide fuel storage and supply during launch and flight. Due to the high technical requirements for these systems, it is important to continuously improve their design and production to ensure high quality and reliability. This article highlights the main aspects of improving the mass sophistication of fuel tanks in RCTs by comparing the classical manufacturing of a wafer tank structure and a composite combination tank. First of all, it discusses the key requirements and standards that are defined for fuel tanks in order to ensure safety and efficiency.The article goes on to analyze the various methods and technologies used to manufacture and control the quality of fuel tanks, including the manufacture of tanks using traditional methods (wafer structures) and composite fuel tank winding. It analyzes the strength and durability of both designs and provides practical recommendations for the development of composite products. Finally, it highlights potential challenges and prospects for development in this area, such as the introduction of new materials, improved manufacturing processes, and the introduction of the latest numerical modeling techniques. Analysis and research of these issues can further improve the mass sophistication of fuel tanks in rocket and space technology and increase the overall reliability of space missions