Ground launch complex for prelaunch preparation and launch carrier rockets from the space head part (optional)

摘要

The invention relates to space engineering. Ground launch facility in each embodiment comprises a freight installation unit (3), the starting structure (4), single-slope gazootrazhatel (4a) with a venting channel, a starting system (5), the cable-filling mast (6), an upper cable mast (7 ) lower mast cable (7a), service tower (8), cabin services (9), a system of charging okisletelem (10) and a system zapraki fuel (11), the cooling system of the fuel (12), equipment gas store (13) refrigerant center (14), temperature control system low pressure air (15), general technical chem we have (16) and auxiliary equipment (17). Ground launch pad additionally provided with a system of temperature control high pressure air, which includes associated with gas storage equipment (13) main pipeline (18), the receiver (19), cylinders (20) which through the charge shield (21) and the conduit (22) a valve connected to the main pipe (18). Shield dispensing (23) of the receiver (19) is connected to the conduit (24) supplying air to space the head (2) provided with a sampling unit (25) connected to the counter (26) of the aerosol particles, control pnevmoschitam (27), remote control means temperature (28) and pressure (29) and a hygrometer (30). In the first embodiment, a system for temperature control of high pressure air space head portion, and the second - thermostating system high pressure air missile compartments - the carrier. AT; third embodiment of a system for high pressure compartments launcher thermostating nitrogen. All versions of the utility model aimed at improving the reliability and efficiency of ground launch complex and ensuring high reliability with launches of CHS. 3 NP of formula