F213_O2S-1_D280SS_L017.jpg F213 O2S-1 D280SS L001ThumbnailsF213 O2S-1 D280SS L018F213 O2S-1 D280SS L001ThumbnailsF213 O2S-1 D280SS L018
"3. REUSABLE SPACE TRANSPORTATION SYSTEM BASED ON A LAUNCH VEHICLE AND AN ORBITAL ANALOGUE MTKS-O AIRCRAFT
Volumes 1 and 3 of the technical proposals outline the feasibility of creating a large-scale analogue of the MTKS orbital aircraft (scale between 1:2.5 and 1:3.5) for experimental confirmation in full-scale conditions of the correctness of technical solutions for an orbital aircraft, including:

- hydrodynamic characteristics and optimality of the layout scheme;
- thermal conditions at atmospheric entry and reliability of heat protective coating;
- inspections and fine-tuning of aircraft design solutions;
- verification of basic and schematic solutions of the hearing control system, etc.
- The launch of the OK analog into the [ISZ] orbit can be carried out by the RLA-120 carrier rocket specially modified for this purpose.

3.I. Possibilities of using MTKS-O for practical purposes

When limiting what is allowed during launch of the launch vehicle RLA-I20 winds at an altitude of 8-12 km to 25-30 m/s and orbital inclination 50.70 the mass of the analog ~26 t turns out to be sufficient to solve certain practical tasks in the ISS orbit in the interests of the Ministry of Defense, National Economy and Science. However, in the main orbit with an inclination of 97°, the analogue cannot be used for practical purposes. (see Fig.1 page 20)."

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