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액체 질소로 윤활되는 극저온 하이브리드 스러스트 베어링 성능 측정
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| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | 류근 | - |
| dc.date.accessioned | 2025-04-01T06:31:46Z | - |
| dc.date.available | 2025-04-01T06:31:46Z | - |
| dc.date.issued | 2022-11-24 | - |
| dc.identifier.uri | https://scholarworks.bwise.kr/erica/handle/2021.sw.erica/122638 | - |
| dc.description.abstract | In this study, the static load characteristics of hybrid thrust bearings for liquid rocket engine turbopumps is present. The test bearing uses liquid nitrogen up to 8 bar(g) as a test fluid. The bearing flow rate and fluid film thickness are measured. | - |
| dc.language | 한국어 | - |
| dc.language.iso | KOR | - |
| dc.title | 액체 질소로 윤활되는 극저온 하이브리드 스러스트 베어링 성능 측정 | - |
| dc.type | Conference | - |
| dc.citation.title | 한국추진공학회 2022년도 제59회 추계학술대회 논문집 | - |
| dc.citation.startPage | 1 | - |
| dc.citation.endPage | 2 | - |
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