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2 139 228

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IPC

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Application

96104872/28, 1996-03-12

(22)

Actual filing date

1996-03-12

(45)

Published

1999-10-10

(72)

Inventor

Akchurin V.P.Zagar O.V.Kalinina V.A.Legostaj I.V.Turkenich R.P.Shalginskij V.M.

(73)

Holder

Nauchno-Proizvodstvennoe Ob"Edinenie Prikladnoj Mekhaniki

TEMPERATURE CONTROL SYSTEM OF SPACECRAFT THERMAL MOCK-UP Russian patent published in 1999 - IPC

Abstract RU 2139228 C1

FIELD: space engineering; temperature control systems of spacecraft thermal mock-ups. SUBSTANCE: according to invention, system includes hydraulic unit with devices for measuring the flow rate and pressure of heat-transfer agent in liquid passage mounted in pressurized container equipped with volume compensator and liquid flow regulating valve (which is fitted before radiator and is provided with one inlet and two outlets) and liquid control instruments panels mounted on the outside of pressurized container. System consists of two modules with hydraulic connectors mounted at inlet and outlet of liquid passages: varying composition module including liquid control instrument panels and compensator and constant composition module with pressurized container, hydraulic unit, volume compensator and radiation fitted with regulating valve whose outlet are connected with radiator inlet through adjustable throttle valves and with its own inlet through check valves. For testing each new spacecraft, only module of varying composition and thermal simulators of instruments are manufactured and filled compensator is connected to one of hydraulic connected. EFFECT: facilitated manufacture and improved service characteristics of temperature control system. 2 cl, 2 dwg

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RU 2 139 228 C1

Authors

Akchurin V.P.

Zagar O.V.

Kalinina V.A.

Legostaj I.V.

Turkenich R.P.

Shalginskij V.M.

Dates

1999-10-10—Published

1996-03-12—Filed

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