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Publikováno v:
Проблемы машиностроения; Том 23, № 3 (2020); 27-36
Проблеми машинобудування; Том 23, № 3 (2020); 27-36
Journal of Mechanical Engineering; Том 23, № 3 (2020); 27-36
Проблеми машинобудування; Том 23, № 3 (2020); 27-36
Journal of Mechanical Engineering; Том 23, № 3 (2020); 27-36
A technique has been developed for reducing the material intensity of highly stressed tail sections of launch vehicles, taking into account strength and stability constraints as well as technological requirements. A cylindrical longitudinally and tra