| 摘要 |
The invention relates to the engine systems of space transportation means. The method is carried out with the aid of a system which comprises a space craft (KLA) with a propulsive jet engine (1) and a device (2) for storing a working substance (one of a fuel components). The system is also provided with a flying fueling apparatus (3) with a system for throwing a working substance (another fuel component). The system (4) forms a stabilized jet (5) of the working substance by means of one or more linear elements (threads, ribbons etc) or on the base of concentrated liquids and solid materials. As a result, a cord (5) for multiple or single use is formed. According to the method, the KLA with the propulsive jet engine (1) and the flying fueling apparatus (3) with the working substance reserve are first launched. At a desired altitude, the working substance is ejected, from the flying fueling apparatus (3), in the form of the cords (5) the density of which is greater than the density of the environmental air. Furthermore, the flying fueling apparatus and the space craft approach each other with a speed which is greater than the speed of the working substance ejection. The cords (5) enter the propulsive jet engine (1) in which the fuel components are mixed and burned up, thereby producing thrust (under conditions that the pulse of combustion products exiting from the nozzle of the jet engine (1) is greater that the pulse of the absorbed jets-cords (5)). The technical result of the group of inventions is directed at reducing costs for transporting cargo to the space. |
