DEVICE FOR STABILISATION OF TEMPERATURE MODE IN PROCESS OF PRE-START PREPARATION OF SPACE HEAD PART WITH ROCKET SPEED-UP UNIT Russian patent published in 2010 - IPC B64G1/50 B64G1/48

Abstract RU 2392199 C1

FIELD: power engineering.

SUBSTANCE: device comprises boxy aprons (7) fixed by their one side to separate part of split joints (6) of rocket speed-up unit (3) in process of pre-start preparation. Sealant (8) with slots is fixed to opposite side of each apron (7). Part of sealant with slots rests on mount (10) of speed-up unit (3) hatch (5). Slots provide for sealant adjacency to hatch mount along its perimeter. Flow of thermostatting air is used to press sealant (8) to mount (10) of hatch and to prevent excessive exhaust of air through hatch.

EFFECT: stabilisation of temperature mode in process of pre-start preparation in cavities of space head part and rocket speed-up unit with hatches open in rocket speed-up unit after connection of mechanisms for withdrawal of split joints.

3 dwg

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RU 2 392 199 C1

Authors

Erpylev Vladimir Vladimirovich

Rozhkov Mikhail Viktorovich

Dates

2010-06-20—Published

2009-04-13—Filed