Zobrazeno 1 - 10
of 35
pro vyhledávání: '"Soon-Sam Hong"'
Publikováno v:
Volume 1: Fluid Applications and Systems; Fluid Measurement and Instrumentation.
The thermodynamic effects on the suction performance of a liquid oxygen (LOX) pump, observed during liquid rocket engine combustion tests, were investigated. Owing to the pump rotational speed and inlet pressure variation in the short duration of the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::793da0fdfcc2d26ed8f45104bd0371b0
https://doi.org/10.1115/fedsm2020-20062
https://doi.org/10.1115/fedsm2020-20062
Autor:
Soon-Sam Hong, Chang-Ho Choi
Publikováno v:
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 60:230-234
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::512dc60f22d244e80dc736a1a62c7cd3
https://doi.org/10.2322/tjsass.60.230
https://doi.org/10.2322/tjsass.60.230
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:
Journal of the Korean Society of Propulsion Engineers. 19:89-95
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8ef9bddacf58159dc23881621a6a01de
https://doi.org/10.6108/kspe.2015.19.3.089
https://doi.org/10.6108/kspe.2015.19.3.089
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
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science. 227:470-480
This article describes a series of development tests of a turbopump, which can be applied to a gas generator cycle rocket engine with liquid oxygen and kerosene propellants. A turbine drives both an oxidizer pump and a fuel pump in the turbopump asse
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::04f71606ab534a0c41a8296b4924d817
https://doi.org/10.1177/0954406212464614
https://doi.org/10.1177/0954406212464614
Autor:
Reza S. Abhari, Soon-Sam Hong
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy. 226:963-974
To see the tip clearance effect on a centrifugal compressor, time-resolved flow measurements are carried out at the discharge of a centrifugal compressor impeller with a diameter of 280 mm. The impeller is 30° back swept and is operated at a blade t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::371b370f2e60fb5b129559ff53395e2c
https://doi.org/10.1177/0957650912455386
https://doi.org/10.1177/0957650912455386
Critical Speed Analysis of a 75 Ton Class Liquid Rocket Engine Turbopump due to Load Characteristics
Publikováno v:
Journal of the Korean Society of Propulsion Engineers. 16:42-49
․ Hyun D. Kwak* ․ Soon-Sam Hong* ․ Jinhan Kim**ABSTRACT Critical speed of high thrust liquid rocket engine turbopump is obtained through a rotordynamic analysis and a unloaded turbopump test is peformed for validation of the numerical model. Th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3a8e57285fc9e2344d5c133a91b67c32
https://doi.org/10.6108/kspe.2012.16.4.042
https://doi.org/10.6108/kspe.2012.16.4.042
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science. 227:311-319
A hydraulic performance test is conducted for a fuel pump of a liquid rocket engine turbopump. The pump driven by an electric motor is tested in a water environment. Experimental results indicate that the inducer has a negligible effect on the head a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::eafcf01486e99fdf9b67d313927ea839
https://doi.org/10.1177/0954406212449939
https://doi.org/10.1177/0954406212449939
Publikováno v:
Transactions of the Korean Society of Mechanical Engineers B. 35:1083-1088
효율이 높고 추력 제어가 쉽기 때문에 추력이 큰 발사체에 일반적으로 널리 사용되는 액체로켓 엔진시스템은 추진제의 공급 방법에 따라 가압식 엔진시스템과 터보펌프식 엔진시스템으로
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::913ee3ef5c498ae52ddad59125e9dff6
https://doi.org/10.3795/ksme-b.2011.35.10.1083
https://doi.org/10.3795/ksme-b.2011.35.10.1083