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2 132 806

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Application

96105511/28, 1996-03-20

(22)

Actual filing date

1996-03-20

(45)

Published

1999-07-10

(72)

Inventor

Akchurin V.P.Gladyshev I.F.Zagar O.V.Kozlov A.G.Novolodskij V.P.Khalimanovich V.I.

(73)

Holder

Nauchno-Proizvodstvennoe Ob"Edinenie Prikladnoj Mekhaniki

METHOD OF TESTING SPACE VEHICLE TEMPERATURE-CONTROL SYSTEM Russian patent published in 1999 - IPC

Abstract RU 2132806 C1

FIELD: space engineering; methods of surface tests of spacecraft temperature-control systems. SUBSTANCE: for conducting the tests, compensating device is disconnected from liquid passage of one of units filled with liquid heat-transfer agent and liquid passages are interconnected by hydraulic joints. Prior to disconnecting the compensating device, change of ambient air temperature is measured, after which compensating device is disconnected from unit and liquid passages are interconnected by hydraulic joints within period of time determined depending on magnitude of measured maximum air temperature rise (as compared with minimum magnitude) near system and permissible pressure rise in liquid passage. EFFECT: enhanced reliability of temperature-control system within assigned service life. 1 dwg

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RU 2 132 806 C1

Authors

Akchurin V.P.

Gladyshev I.F.

Zagar O.V.

Kozlov A.G.

Novolodskij V.P.

Khalimanovich V.I.

Dates

1999-07-10—Published

1996-03-20—Filed

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