245 0

재사용 우주발사체용 로켓엔진 터보펌프에 적용하기 위한 극저온 유체 외부가압 베어링과 적층제조기술에 관하여

Title
재사용 우주발사체용 로켓엔진 터보펌프에 적용하기 위한 극저온 유체 외부가압 베어링과 적층제조기술에 관하여
Other Titles
On the Cryogenic Fluid Hydrostatic Bearings and Additive Manufacturing for Rocket Engine Turbopumps of Reusable Launch Vehicles
Author
류근
Keywords
Reusable launch vehicles(재사용 우주발사체); Liquid rocket engines(액체로켓엔진); Hydrostatic bearings(외부가압 베어링); Fluid film bearings(유체 베어링); Additive manufacturing(적층제조기술)
Issue Date
2019-05
Publisher
한국추진공학회
Citation
한국추진공학회 2019년도 제52회 춘계학술대회 논문집, Page. 482 - 484
Abstract
The present work reviews critical technology development and recent breakthroughs in high-performance cryogenic fluid hydrostatic bearings and additive manufacturing technology for rocket engine turbopumps of reusable launch vehicles and discusses their future challenges and opportunities, as well as technical obstacles.
URI
http://www.dbpia.co.kr/journal/articleDetail?nodeId=NODE09220626&language=ko_KRhttps://repository.hanyang.ac.kr/handle/20.500.11754/113649
Appears in Collections:
COLLEGE OF ENGINEERING SCIENCES[E](공학대학) > MECHANICAL ENGINEERING(기계공학과) > Articles
Files in This Item:
There are no files associated with this item.
Export
RIS (EndNote)
XLS (Excel)
XML


qrcode

Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.

BROWSE