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2 513 324

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IPC

B64G1/50(2006-01-01)

(21) (22)

Application

2012142385/11, 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 PetrovichGolovenkin Evgenij NikolaevichZakharov Sergej AleksandrovichKuznetsov Anatolij Jur'EvichAkchurin Vladimir PetrovichPopugaev Mikhail MikhajlovichGabov 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

Abstract RU 2513324 C1

FIELD: transport.

SUBSTANCE: invention relates to thermal control systems of, mainly, telecommunication satellites. Proposed system comprises closed heat carrier circulation circuit. Said circuit is composed of fluid circuits of electrically driven pump unit, manifolds of radiator panels, metre panels and connection pipes. Length of said fluid circulation circuit has two parallel different-length branches. Smaller-length branch features smaller ID. Total length of said sections is calculated by definite mathematical formula.

EFFECT: decreased sizes, higher reliability.

3 dwg

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RU 2 513 324 C1

Authors

Khalimanovich Vladimir Ivanovich

Lavrov Viktor Ivanovich

Kolesnikov Anatolij Petrovich

Golovenkin Evgenij Nikolaevich

Zakharov Sergej Aleksandrovich

Kuznetsov Anatolij Jur'Evich

Akchurin Vladimir Petrovich

Popugaev Mikhail Mikhajlovich

Gabov Aleksej Sergeevich

Dates

2014-04-20—Published

2012-10-04—Filed