| 摘要 |
The invention relates to aerospace technology and can be used, in particular, to place different payloads, such as communication, navigation, monitoring satellites (including ecology monitoring satellites), and scientific instruments, into low and medium earth orbits, as well as to promptly deliver payloads to remote terrestrial and oceanic areas. An aerospace system is proposed, which comprises a carrier aircraft 1, a launch vehicle 2 and a payload 3. The launch vehicle 2 with liquid fuel propulsion units 4 is placed inside a fuselage 5 of the carrier aircraft 1 within a transport and launch container 6 with the aid of support units 12 in at least in two areas, an airtight pneumatic chamber 14 is formed between the blind end 13 of the transport and launch container 6 and the end of the launch vehicle 2, which chamber incorporates airborne elements of units 8 for supplying the launch vehicle with propellant and working mediums, elements of a draining unit 9, elements of a unit 10 for replenishing the liquid fuel propulsion units with propellant, electrical connections 11, wherein all said units 9, 10, electrical connections 11 and airborne elements 8 are connected to the end of the launch vehicle 2 by pull-off couplings 15, wherein the transport and launch container is provided with a pneumatic ejection unit 7, made in the form of a high pressure source 16 connected by stop valves 17 to the pneumatic chamber 14 and positioned in the transport and launch container 6, provided with thermal insulation 18, wherein the diameter of the free end 19 the container 6, provided with a frangible membrane 20, is hermetically connected to the perimeter of the port in the fuselage 5 of the carrier aircraft 1. The proposed system makes it possible to enhance payload capacity and to reduce the specific cost of putting a payload in orbit, to provide a high degree of safety for the carrier aircraft and its crew, and also to ensure ecological safety of the system. <IMAGE> |
