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2 485 028

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IPC

B64G1/50(2006-01-01)

(21) (22)

Application

2011133112/11, 2011-08-05

(24)

Start date

2011-08-05

(22)

Actual filing date

2011-08-05

(45)

Published

2013-06-20

(72)

Inventor

Khalimanovich Vladimir IvanovichLavrov Viktor IvanovichKolesnikov Anatolij PetrovichTsivilev Ivan NikolaevichPopov Aleksej ViktorovichShajbin Artem OlegovichGanenko Sergej AlekseevichVolovikov Vitalij GavrilovichAkchurin Vladimir Petrovich

(73)

Holder

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

METHOD OF CONTROL OVER SPACECRAFT THERMAL CONTROL SYSTEM Russian patent published in 2013 - IPC B64G1/50

Abstract RU 2485028 C2

FIELD: transport.

SUBSTANCE: invention relates to thermal control systems of, mainly, telecommunication satellites. Proposed method comprises periodical telemetry measurements of gas temperature in tight container and rpm of fan motor mounted therein. Gas pressure in tight container is defined from gas temperature measured by remote means with the help of transducers and said motor rpm. Note here that that data are used obtained in preliminary independent fan tests describing the rpm-to-gas pressure ratio.

EFFECT: higher reliability, decreased weight and lower power consumption.

3 dwg

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RU 2 485 028 C2

Authors

Khalimanovich Vladimir Ivanovich

Lavrov Viktor Ivanovich

Kolesnikov Anatolij Petrovich

Tsivilev Ivan Nikolaevich

Popov Aleksej Viktorovich

Shajbin Artem Olegovich

Ganenko Sergej Alekseevich

Volovikov Vitalij Gavrilovich

Akchurin Vladimir Petrovich

Dates

2013-06-20—Published

2011-08-05—Filed