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2 564 286

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IPC

B64G1/50(2006-01-01)

G05D1/08(2006-01-01)

(21) (22)

Application

2012142382/11, 2012-10-04

(24)

Start date

2012-10-04

(22)

Actual filing date

2012-10-04

(45)

Published

2015-09-27

(72)

Inventor

Khalimanovich Vladimir IvanovichLavrov Viktor IvanovichKolesnikov Anatolij PetrovichGolovenkin Evgenij NikolaevichDostavalov Aleksandr ValentinovichVolovikov Vitalij GavriilovichAkchurin Georgij VladimirovichPopugaev Mikhail Mikhajlovich

(73)

Holder

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

SPACECRAFT THERMAL CONTROL SYSTEM Russian patent published in 2015 - IPC B64G1/50 G05D1/08

Abstract RU 2564286 C2

FIELD: heating.

SUBSTANCE: invention relates to thermal regulation systems (TRS) of spacecrafts (S), mainly telecommunication satellites. TRSs of such Ss contains the identical duplicated liquid loops for the heat carrier. The loops comprise the liquid paths nearby and are fitted with hydraulic pumps with close flow rate and pressure head characteristics. The layout of connection of liquid paths with hydraulic pumps is implemented so that the directions of movement of the heat carrier in the neighbouring liquid paths are mutually opposite.

EFFECT: reduction of total uncompensated kinetic moment from the working TRS and ensuring, thereby, the decrease of flow rate of working body of orientation and stabilisation system of S.

6 dwg

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RU 2 564 286 C2

Authors

Khalimanovich Vladimir Ivanovich

Lavrov Viktor Ivanovich

Kolesnikov Anatolij Petrovich

Golovenkin Evgenij Nikolaevich

Dostavalov Aleksandr Valentinovich

Volovikov Vitalij Gavriilovich

Akchurin Georgij Vladimirovich

Popugaev Mikhail Mikhajlovich

Dates

2015-09-27—Published

2012-10-04—Filed