FIELD: transport.
SUBSTANCE: invention relates to space engineering. Proposed device comprises pipeline 5, assembly to transfer container via pipeline and assembly to prepare and load container. The latter comprises rotary support 8 arranged on fixed support 7, bush 18 to accommodate container 17 and container cover 18. Transfer assembly comprises housing 19 accommodating gas-tight sleeve 20 representing, in initial position, a flat tape. Sleeve open end is tightly jointed with housing 19. Space 22 is communicated via air line 11 and start-and-shut-ff valve 12 with compressed gas source 10. Bush 16 has spring-loaded flange 24 and is locked by pyro cotter 27. Cover 18 is locked by pyro cotter 28. Support 8 is also locked by pyro cotter and provided with spring pusher 31 with rod 32 to displace transfer assembly, together with bush 16 and container 17, to under cover 18. Pyro cotter 27 operated, container 17 is closed by cover 18. Pyro cotter 28 and valve 12 operated, sleeve 20, straightening under gas pressure, displaces container 17 along pipeline 5. Delivery of container into autolander from any direction.
EFFECT: higher versatility of proposed device.
9 cl, 6 dwg
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Authors
Dates
2011-03-10—Published
2010-03-18—Filed