Komarov

The article describes a comparative analysis and economical efficiency estimates for the two considered ways of low -dimensional spacecraft low orbit insertion: the traditional one, using the traditional rocket launch systems, and the perspective one, using the ballistic active-reactive system. The conducted research is preliminary and as the accumulation of more source data of active-ballistic rocket systems technology goes, is subject to change, but at this stage it can serve as a basis for further analysis and evaluation of possible design. Economic efficiency of payload delivery using the ballistic active-reactive system in the given formulation of the problem is preferable.

 The article shows the importance of a single complex efficiency criterion for innovative projects, which is centrally approved, and will allow an a priori evaluation of projects in indeterminacy typical to early stages of development. The criterion of efficiency not overloaded with a considerable quantity of parameters reflects target directivity of the task (operation) and in the conditions of restrictions and superimposed uncertainties allows solving so-called "direct" research problems of operations which help to create formation of programs from engineering positions.

In this article the approach is considered, allowing to adapt for the developed now and predicted organization, engaged in experimental rocket complexes. The methodical approach offered in article is based on use during the experimental working off a rocket complex’s quantitative estimation indicators of reliability during the development of operating influences and allows to consider and compensate the revealed defects and to increase the experimental working off of rocket complexes’ efficiency as a whole.