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2 221 732

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Application

2001111915/11, 2001-04-27

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Start date

2001-04-27

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Actual filing date

2001-04-27

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Published

2004-01-20

(72)

Inventor

Akchurin V.P.Alekseev N.G.Butkina N.F.Nikitin V.N.Petrusevich V.G.Shilkin O.V.

(73)

Holder

Federal'Noe Gosudarstvennoe Unitarnoe Predprijatie Ob"Edinenie Prikladnoj Mekhaniki Im. Akad. M.F.Reshetneva"

SPACECRAFT TEMPERATURE CONTROL SYSTEM Russian patent published in 2004 - IPC

Abstract RU 2221732 C2

FIELD: space engineering; temperature control systems of communication satellites. SUBSTANCE: input of standby flow regulator of proposed system is communicated via sensitive elements of main and auxiliary thermoregulators with output of liquid instrument panel. Second output of standby thermo-regulator is connected with input and first output is connected with first output of main thermo-regulator and then with inlet of bypass valve. Second and first outlets of said valve are communicated with inlet of satellite radiator through liquid passage of panel mounted on satellite and directed to Sun. EFFECT: simplified construction; reduced power requirements. 3 dwg

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RU 2 221 732 C2

Authors

Akchurin V.P.

Alekseev N.G.

Butkina N.F.

Nikitin V.N.

Petrusevich V.G.

Shilkin O.V.

Dates

2004-01-20—Published

2001-04-27—Filed

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