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IPC

B64G1/50(2006-01-01)

B64G5/00(2006-01-01)

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Application

2013117839/11, 2013-04-17

(24)

Start date

2013-04-17

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Actual filing date

2013-04-17

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Published

2015-01-10

(72)

Inventor

Khalimanovich Vladimir IvanovichGolovenkin Evgenij NikolaevichSorokvasha Gennadij Grigor'EvichKolesnikov Anatolij PetrovichAnkudinov Aleksandr VladimirovichAkchurin Georgij VladimirovichVolovikov Vitalij GavriilovichShilkin Oleg ValentinovichAkchurin Vladimir Petrovich

(73)

Holder

Otkrytoe Aktsionernoe Obshchestvo Sputnikovye Sistemy" Imeni Akademika M.F. Reshetneva"

METHOD OF MANUFACTURING OF SPACECRAFT THERMAL CONTROL SYSTEM Russian patent published in 2015 - IPC B64G1/50 B64G5/00

Abstract RU 2538828 C2

FIELD: aviation.

SUBSTANCE: according to the invention the liquid loop of the thermal control system for ground tests is charged with liquid heating medium, in particular solvent. Then the heating medium is drained by air purging till its complete removal prior to vacuum drying. The later precedes the thermal control system charging with actual heating medium. At that initially the entire liquid line is purged bypassing (by means of the bypass line control valve) the specified vertical heads of the radiator panels. These headers are purged after all the others (switching the control valve to another position).

EFFECT: increased produceability of the thermal control system and reducing time of purging during the heating medium drainage.

3 dwg

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RU 2 538 828 C2

Authors

Khalimanovich Vladimir Ivanovich

Golovenkin Evgenij Nikolaevich

Sorokvasha Gennadij Grigor'Evich

Kolesnikov Anatolij Petrovich

Ankudinov Aleksandr Vladimirovich

Akchurin Georgij Vladimirovich

Volovikov Vitalij Gavriilovich

Shilkin Oleg Valentinovich

Akchurin Vladimir Petrovich

Dates

2015-01-10—Published

2013-04-17—Filed