Zobrazeno 1 - 4
of 4
pro vyhledávání: '"Jun-Hwan Bae"'
Autor:
Jun Hwan Bae, Bong Kyu Sun
Publikováno v:
The Journal of Humanities and Social sciences 21. 9:455-468
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ae52955648a660f09e944dba49398ca4
https://doi.org/10.22143/hss21.9.1.36
https://doi.org/10.22143/hss21.9.1.36
Autor:
Chang-Ho Choi, Hyun-Duck Kwak, Min-Ju Park, Daejin Kim, Seong-Lyong Kim, Seong-Min Jeon, Soon-Sam Hong, Jun-Hwan Bae, YeongMin Han, Suck-Hwan Yoon, Eun-Hwan Jeong, Hang-Gi Lee, Ju Hyun Shin, Pyun-Goo Park, Seong-Phil Woo, Jin-Sun Kim, Jun-Gu Noh, Jin-Han Kim, Seung-Han Kim, Seong-Won Wang
Publikováno v:
Journal of the Korean Society of Propulsion Engineers. 20:86-93
Performance tests of a 75-tonf liquid rocket engine turbopump were conducted. The performance of sub-components - two pumps and a turbine - and their power matching were measured and examined firstly near the design speed under the LN2 and kerosene e
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::146306047f058f54dedf8590128c9c8f
https://doi.org/10.6108/kspe.2016.20.2.086
https://doi.org/10.6108/kspe.2016.20.2.086
Publikováno v:
Volume 2B: Turbomachinery.
This study investigates the behavior of a turbopump assembly during critical cavitation of the propellant pumps in the upper rocket engine of the Korea Space Launch Vehicle-II. Turbopumps operate under conditions involving low pressure at the pump in
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b385a6f167c396a253e7f0ddcab39b06
https://doi.org/10.1115/gt2018-76430
https://doi.org/10.1115/gt2018-76430
Autor:
Jin-Han Kim, Eun-Hwan Jeong, YeongMin Han, Hang-Gi Lee, Suck-Hwan Yoon, Chang-Ho Choi, Jin-Sun Kim, Ju Hyun Shin, Jun-Gu Noh, Jun-Hwan Bae, Seong-Min Jeon, Soon-Sam Hong, Daejin Kim, Seung-Han Kim, Seong-Lyong Kim, Hyun Duck Kwak, Pyun-Goo Park
Publikováno v:
Journal of the Korean Society of Propulsion Engineers. 19:65-72
Performance tests of a turbopump for the developing 7-tonf li quid rocket engine were conducted. The performance of turbopump components and their power matchin g were measured and examined firstly under the LN2 and water environment.. In the real pr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2163d7969a2a225727a3ce74a73ac433
https://doi.org/10.6108/kspe.2015.19.2.065
https://doi.org/10.6108/kspe.2015.19.2.065