FIELD: rocketry and space engineering.
SUBSTANCE: proposed launching complex of each design version contains transportation-and-assembly package 3, launch facility 4, launch system 5, umbilical mast 6, upper cable mast 7, service tower 8, service cabin 9, oxidizer filling system 10 and fuel filling system 11, fuel cooling system 12, gas storage equipment 13, cooling center 14 and low air pressure thermostatic control system 15 of nose cone 2. Launching complex is furnished with thermostatic control system including main pipeline 18, receiver 19 and bottles 20 of which are connected with main pipeline 18 through charging panel 21 and pipeline 22 with valves, all connected with gas storage equipment 13. Delivery panel 23 of receiver 19 is connected with air delivery pipeline 24 provided with sampler 25 connected with aerosol particles counter 26, pneumatic control panel 27, temperature and pressure remote control devices and hygrometer 30 according to first design version, high air pressure thermostatic control system is provided in nose cone 2. According to second design version, high air pressure thermostatic control system of launch vehicle compartment is provided. According to third design version, nitrogen high pressure thermostatic control system of launch vehicle compartments is provided.
EFFECT: improved reliability and efficiency of operation of launching complex.
4 cl, 4 dwg
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