F213_O2S-1_D280SS_L018.jpg F213 O2S-1 D280SS L017ThumbnailsF213 O2S-1 D280SS L019F213 O2S-1 D280SS L017ThumbnailsF213 O2S-1 D280SS L019
"In this regard, at the preliminary design stage, the possibilities and feasibility of using an OS analogue in orbits with an inclination of 97° and an altitude of up to 400 km should be considered. If this issue is resolved positively, the scope of modifications to the RLA-120 launch vehicle, specific tasks that the system can solve, based on the characteristics of the OS analogue and the conditions for launching the launch vehicle, must also be determined."

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