FIELD: chemistry.
SUBSTANCE: invention is referred to means of matching and separation of pneumohydraulic systems of space objects (SO). The detachable device has forwarding studs (1) with fixing elements and division gears. Studs may be fixed on a detached part (9) of the SO, and fixing elements - on the core vehicle (11) of the SO, and division gears (engines) - on the launch vehicle. Transit line is equipped with the first (4) and the second (5) adapters which form a detachable joint in the shape of adapter (4) top (6) and adapter (5) flange (7). The top (6) enters the flange (7) core space, and their joint is sealed with inserts (8). The adapter (5) is attached to the detached part (9) of the SO with the help of a flange (7) and fixturing components (10), and the adapter (4) is fixed on the core vehicle (11) of the SO with a pylon (12). Supporting part (13) of the pylon is fixed on the core vehicle (11) of the space object with the help of elements (10), and an adjustable part (14) - on the screwed shank (15) of the adapter (4) with the screw nuts (16). Oval holes (17) provide regulation of relative position of the parts (12) and (14) on installation sites of fixturing elements (10). Displacement of the pylon (12) in relation to the adapter (4) is fixed with two screw nuts (16) by means of their screwing along the tail (15). Studs (1) cylinder part (18) is longer than disconnection stroke of adapters (4) and (5). Thus, deformation by the disconnection is not possible. After SO parts connection, the adapter (5) is fixed on the detached part (9). Then the first adapter (4) is attached to it and it the pylon (12) is installed on it. The pylon (12) is fixed on the core vehicle (11). Then transit pipelines are attached to the adapters and adapters' conjunctions are technologically unfixed.
EFFECT: increased safety of the detached device by minimal mass expenses.
2 cl, 3 dwg
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Authors
Dates
2012-02-10—Published
2010-08-16—Filed