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RU

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2 447 000

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C2

(51)

IPC

B64G1/50(2006-01-01)

B64G5/00(2006-01-01)

(21) (22)

Application

2010119382/11, 2010-05-14

(24)

Start date

2010-05-14

(22)

Actual filing date

2010-05-14

(45)

Published

2012-04-10

(72)

Inventor

Bartenev Vladimir Afanas'EvichKhalimanovich Vladimir IvanovichZagar Oleg VjacheslavovichTurkenich Roman PetrovichAkchurin Vladimir Petrovich

(73)

Holder

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

SPACECRAFT THERMAL CONTROL SYSTEM Russian patent published in 2012 - IPC B64G1/50 B64G5/00 

Abstract RU 2447000 C2

FIELD: transport.

SUBSTANCE: invention relates to thermal control systems (TCS) mainly, of telecommunication satellites, to their manufacture and ground tests. TCS comprises fluid circuits of instrumentation panels, hydraulic pump, hydraulic accumulator, temperature pickups, shutoff valve and two onboard outer gate valves. The latter communicate with inlet and outlet of the system plug-in equipment fluid circuit including fluid-to-fluid heat exchanger, flow rate meters, those of pressure and temperature. Inlet and outlet of the system plug-in equipment fluid circuit are connected to said outer gate valves via adapters. Adapters are connected to free unions of outer gate valves by threaded joint. Opposite ends of said adapters terminate in hydraulic joints and are jointed with hydraulic joints of flexible metal pipelines. These pipelines are connected with inlet and outlet of plug-in equipment liquid circuit.

EFFECT: simplified manufacture of spacecraft.

3 dwg

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RU 2 447 000 C2

Authors

Bartenev Vladimir Afanas'Evich

Khalimanovich Vladimir Ivanovich

Zagar Oleg Vjacheslavovich

Turkenich Roman Petrovich

Akchurin Vladimir Petrovich

Dates

2012-04-10—Published

2010-05-14—Filed

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