The figures 8, 9, 10, 11, 12, 13, 14, 15, 19, 20, 21, 22, 23 show examples of connections, which scenarios are of real interest for potential customers. The other scenarios determined by concrete tasks are also possible.
Scenario 1 - the regular and revised spacecrafts of class "Soyuz" - TMSC and MNMSC (MNMSC-cargo, MNMSC-MR) are used, pls. see fig fig.8. The term of deployment of small orbital station on this scenario depends on terms of technical readiness of TMSC and MNMSC (i.e. the determining factor by preparation of this plan is the readiness of the production by minimum design and engineering works). Taking into account the revisions of MNMSC, its realization in one year after the beginning of preparation works is possible. The time of operation of MNMSC on the orbit can be extended up to 180 days by some revision of power supply system. In its turn, this will allow to conduct several visiting expeditions "against a background" of one MNMSC and, naturally, to lower.
Scenario 3 - three-element scenario requiring a development of the module (e.g., LM, DM, SPM), pls. see fig. fig.11, 13, 14. The terms of transition to this scenario are determined by terms of readiness of one or another module. It should be noted that the largest readiness for today is observed by the module-spacecraft DM (its approximate manufacturing time is 1,5 years). The least readiness is by LM (the readiness of this module is about three years).
It should be noted that the appearance of connections of SOS what are also of specific interest for customers is possible by the transition from one scenario to another one. As example, by the transition from two-element to three-element scenarios, in particular, by appearance of a connection of TMSC+DM it is possible to arrange "the going out" of a space tourist into the open space, to put a satellite into orbit "manually", to install additional solar batteries in DM. If a connection TMSC+SPMappears, it is possible to conduct experiments with apparatuses of higher power consumption, etc.
The deployment of the station is not limited to scenarios represented above and allows the use of orbital modules put into orbit on other carrier rockets and their modifica