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2 196 084

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IPC

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Application

96105429/28, 1996-03-20

(24)

Start date

1996-03-20

(22)

Actual filing date

1996-03-20

(45)

Published

2003-01-10

(72)

Inventor

Akchurin V.P.Goncharuk V.I.Zagar O.V.Kozlov A.G.Khalimanovich V.I.

(73)

Holder

Nauchno-Proizvodstvennoe Ob"Edenenie Prikladnoj Mekhaniki

SPACECRAFT TEMPERATURE CONTROL SYSTEM Russian patent published in 2003 - IPC

Abstract RU 2196084 C2

FIELD: space engineering; spacecraft temperature control systems. SUBSTANCE: proposed system has gas and liquid passages. Compensating unit with bellows is additionally mounted between filter and heat exchanger of removable equipment of liquid passage. Bellows is fixed in its extreme position and its inlet is connected with second outlet of heat exchanger and outlet is connected with filter inlet. Second inlet of heat exchanger and filter outlet are connected via flexible metal pipe lines with hydraulic joint at the ends. Hydraulic joints are connected with remaining part of liquid passage of system through flexible metal pipe line and flowthrough valve. After ground tests (before launch of spacecraft) removable equipment is dismantled and said joints are coupled together. Flowthrough valve is closed and bellows is unlocked and operates in autonomous mode. EFFECT: enhanced reliability; increased operating time of system; facilitated pre-launch procedure. 4 dwg

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RU 2 196 084 C2

Authors

Akchurin V.P.

Goncharuk V.I.

Zagar O.V.

Kozlov A.G.

Khalimanovich V.I.

Dates

2003-01-10—Published

1996-03-20—Filed

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