Analysis of the Main Design Parameters of an Oxygen-Hydrogen Rocket Unit for Ultra-Light Launch Vehicles
The article provides an analysis of the structural and layout diagrams of oxygen-hydrogen rocket units of ultra-light launch vehicles and their energy capabilities. There are several directions, the implementation of one of which will make it possible to create a family of launch vehicles based on the development of basic rocket units of various mass-dimensional sizes and configurations. This article provides an overview analysis of the state of the art in the development of a number of ultra-light launch vehicles. The questions of definition and selection of mass-energy and volume-geometric ratios of launch vehicles and principles of construction of components of ultra-light launch vehicles are considered. The article discusses the problem of analyzing design and technical solutions in the field of creating the components of an ultra-light launch vehicle using liquid hydrogen as fuel.