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IPC

B64G1/50(2006-01-01)

G05D1/08(2006-01-01)

(21) (22)

Application

2012142387/11, 2012-10-04

(24)

Start date

2012-10-04

(22)

Actual filing date

2012-10-04

(45)

Published

2014-04-20

(72)

Inventor

Khalimanovich Vladimir IvanovichLavrov Viktor IvanovichKolesnikov Anatolij PetrovichDostavalov Aleksandr ValentinovichAkchurin Georgij VladimirovichKnjazev Aleksandr Grigor'EvichGordeev Egor AleksandrovichGabov Aleksej Sergeevich

(73)

Holder

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

SPACECRAFT THERMAL CONTROL SYSTEM Russian patent published in 2014 - IPC B64G1/50 G05D1/08

Abstract RU 2513321 C1

FIELD: transport.

SUBSTANCE: invention relates to thermal control systems of, mainly, telecommunication satellites. Thermal control system comprises closed heat carrier circulation circuit. The latter includes electrically driven pump unit, pressure accumulator, manifolds of control panels and those of radiators. Said elements are interconnected by lengths of connection pipelines with inlet and outlet flow sections complying with those of said elements. Portion of lengths of said connection pipelines feature identical equivalent ID smaller than diameters of the other parts and total length that satisfies the definite relationship.

EFFECT: decreased sizes, higher reliability.

1 dwg

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RU 2 513 321 C1

Authors

Khalimanovich Vladimir Ivanovich

Lavrov Viktor Ivanovich

Kolesnikov Anatolij Petrovich

Dostavalov Aleksandr Valentinovich

Akchurin Georgij Vladimirovich

Knjazev Aleksandr Grigor'Evich

Gordeev Egor Aleksandrovich

Gabov Aleksej Sergeevich

Dates

2014-04-20—Published

2012-10-04—Filed