| 发明名称 |
METHOD OF FILLING SPACECRAFT THERMAL CONTROL SYSTEM HYDRAULIC LINE WITH HEAT CARRIER |
| 摘要 |
FIELD: transport. ^ SUBSTANCE: invention relates space engineering, particularly to method of filling spacecraft thermal control system hydraulic line with heat carrier. Proposed method comprises measuring hydraulic line dry volume, filling pre-evacuated hydraulic line with deaerated heat carrier at surplus pressure, bleeding a portion of heat carrier from spacecraft volume compensator fluid chamber and measuring its volume with the help of reference vessel. Heat carrier portion drained, volume of not-dissolved gas bubbles in hydraulic line is determined from the measurements results. ^ EFFECT: higher reliability. ^ 2 dwg |
| 申请公布号 |
RU2397118(C2) |
申请公布日期 |
2010.08.20 |
| 申请号 |
RU20080139839 |
申请日期 |
2008.10.07 |
| 申请人 |
OTKRYTOE AKTSIONERNOE OBSHCHESTVO "INFORMATSIONNYE SPUTNIKOVYE SISTEMY" IMENI AKADEMIKA M.F. RESHETNEVA" |
发明人 |
TESTOEDOV NIKOLAJ ALEKSEEVICH;KOSENKO VIKTOR EVGEN'EVICH;BARTENEV VLADIMIR AFANAS'EVICH;KHALIMANOVICH VLADIMIR IVANOVICH;DANILOV EVGENIJ NIKOLAEVICH;BLIZNEVSKIJ ALEKSANDR SERGEEVICH;AKCHURIN VLADIMIR PETROVICH;ALEKSEEV NIKOLAJ GRIGOR'EVICH;ZAGAR OLEG VJACHESLAVOVICH;GUPALO VIKTOR KUZ'MICH;VOLOVIKOV VITALIJ GAVRIILOVICH;KOLESNIKOV ANATOLIJ PETROVICH;SERGEEV JURIJ DMITRIEVICH;TRUBKIN PETR IVANOVICH;TURKENICH ROMAN PETROVICH;SHILKIN OLEG VALENTINOVICH |
| 分类号 |
B64G1/50;B67D99/00;G01F23/02 |
主分类号 |
B64G1/50 |
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