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2 698 573

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IPC

B64G1/50(2006-01-01)

(21) (22)

Application

2018119398, 2018-05-25

(24)

Start date

2018-05-25

(22)

Actual filing date

2018-05-25

(45)

Published

2019-08-28

(72)

Inventor

Kolesnikov Anatolij PetrovichLegostaj Igor VasilevichShilkin Oleg ValentinovichAkchurin Vladimir PetrovichDmitriev Gennadij ValerevichMarchenko Igor AnatolevichSvinin Timofej PetrovichOvchinnikov Konstantin VasilevichBakurov Evgenij YurevichSokolov Sergej Nikolaevich

(73)

Holder

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

TEST METHOD OF SPACECRAFT TEMPERATURE CONTROL SYSTEM Russian patent published in 2019 - IPC B64G1/50

Abstract RU 2698573 C1

FIELD: astronautics.

SUBSTANCE: invention relates to space engineering, particularly, to ground-based testing of space systems. Test method of spacecraft temperature control system includes the following actions. Filling of system paths with liquid heat carrier. Undocking of compensation device. Connection of fluid circuit with fluid circuit of service systems module with standard volume compensator. Heat carrier dose is drained from the volume compensator fluid cavity. At that, from the liquid cavity of the compensating device during draining, the heat carrier dose is measured, which is determined as per the specified ratio taking into account the volume of the compensation device and the maximum volume expansion of the heat carrier in the fluid circuits.

EFFECT: enabling higher reliability.

1 cl, 8 dwg

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RU 2 698 573 C1

Authors

Kolesnikov Anatolij Petrovich

Legostaj Igor Vasilevich

Shilkin Oleg Valentinovich

Akchurin Vladimir Petrovich

Dmitriev Gennadij Valerevich

Marchenko Igor Anatolevich

Svinin Timofej Petrovich

Ovchinnikov Konstantin Vasilevich

Bakurov Evgenij Yurevich

Sokolov Sergej Nikolaevich

Dates

2019-08-28—Published

2018-05-25—Filed