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2 269 457

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(51)

IPC

B64G1/22(2006-01-01)

B64G1/50(2006-01-01)

(21) (22)

Application

2003137712/11, 2003-12-26

(24)

Start date

2003-12-26

(22)

Actual filing date

2003-12-26

(45)

Published

2006-02-10

(72)

Inventor

Kozlov Al'Bert GavrilovichBartenev Vladimir Afanas'EvichKesel'Man Gennadij DavydovichShelud'Ko Vjacheslav Grigor'EvichKhalimanovich Vladimir IvanovichMikhnev Mikhail MikhajlovichAkchurin Vladimir PetrovichAkchurin Georgij VladimirovichBliznevskij Aleksandr SergeevichRoskin Sergej MikhajlovichGolovenkin Evgenij NikolaevichTurkenich Roman PetrovichGupalo Viktor Kuz'MichZagar Oleg VjacheslavovichShilkin Oleg ValentinovichDmitriev Gennadij Valer'Evich

(73)

Holder

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

METHOD OF MANUFACTURE OF PAYLOAD MODULE FOR SPACECRAFT Russian patent published in 2006 - IPC B64G1/22 B64G1/50

Abstract RU 2269457 C2

FIELD: space engineering; manufacture of communication satellites.

SUBSTANCE: proposed method includes testing the payload for serviceability. To this end, technological compensating device is connected to module before and after tests. Gas cavity of this device is preliminarily filled with gas under pressure and definite amount of heat-transfer agent is drained from liquid cavity. Pressure and amount of liquid being drained are selected in definite ratio.

EFFECT: reduction of rejects, hidden rejects inclusive.

2 dwg

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RU 2 269 457 C2

Authors

Kozlov Al'Bert Gavrilovich

Bartenev Vladimir Afanas'Evich

Kesel'Man Gennadij Davydovich

Shelud'Ko Vjacheslav Grigor'Evich

Khalimanovich Vladimir Ivanovich

Mikhnev Mikhail Mikhajlovich

Akchurin Vladimir Petrovich

Akchurin Georgij Vladimirovich

Bliznevskij Aleksandr Sergeevich

Roskin Sergej Mikhajlovich

Golovenkin Evgenij Nikolaevich

Turkenich Roman Petrovich

Gupalo Viktor Kuz'Mich

Zagar Oleg Vjacheslavovich

Shilkin Oleg Valentinovich

Dmitriev Gennadij Valer'Evich

Dates

2006-02-10—Published

2003-12-26—Filed