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"3. JUSTIFICATION OF THE PRINCIPAL LAYOUT OF THE MTKS

The basic layout diagram significantly affects the geometric and mass characteristics of the launch system.

The following general requirements apply to its selection:

ensuring minimal costs for development and production;
maximum degree of use of standardized components and assemblies;
taking into account the technical capabilities of the existing production base.

The decisive moment for the construction of the entire reusable transport space system is the choice of the layout scheme of the orbital aircraft.

3.I. Orbital aircraft layout

The layout of the orbital aircraft (OS) is determined by the basic requirements given in Section 2.
The implementation of these requirements clearly determines the need to use an aircraft design [2]. The peculiarity of the aerodynamic configuration is due to the operation of the OS in a wide range of speeds (0.5
The use of the OS as a universal vehicle with the aim of reducing the impact of external factors on the launched and returned payload determines the need for internal [cont.]"

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