| 发明名称 |
METHOD OF MANUFACTURE OF PAYLOAD MODULE FOR SPACECRAFT |
| 摘要 |
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 |
| 申请公布号 |
RU2269457(C2) |
申请公布日期 |
2006.02.10 |
| 申请号 |
RU20030137712 |
申请日期 |
2003.12.26 |
| 申请人 |
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发明人 |
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 |
| 分类号 |
B64G1/00;B64G1/22;B64G1/50 |
主分类号 |
B64G1/00 |
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