Zobrazeno 1 - 10
of 12
pro vyhledávání: '"Berlin Huang"'
Autor:
Berlin Huang, 黃柏霖
93
Low-thrust bipropellant propulsion systems are mainly applied on the attitude and altitude controls of satellites. The hypergolic phenomenon of NTO/MMH impingement constructs the required combustion for thrust generation and the flame tempera
Low-thrust bipropellant propulsion systems are mainly applied on the attitude and altitude controls of satellites. The hypergolic phenomenon of NTO/MMH impingement constructs the required combustion for thrust generation and the flame tempera
Externí odkaz:
http://ndltd.ncl.edu.tw/handle/96329878241480720440
Autor:
Tony Yuan, Berlin Huang
Publikováno v:
Atomization and Sprays. 22:391-408
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::907fa2a174e88b33d5f0c84379c891b7
https://doi.org/10.1615/atomizspr.2012005547
https://doi.org/10.1615/atomizspr.2012005547
Publikováno v:
Journal of Propulsion and Power. 27:509-512
T HE miniaturization of space systems, such as microsatellites, has become an important development trend. Using a cluster of microspacecraft with a constellational architecture to replace a traditional spacecraft can greatly reduce the costs of prod
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1b4959aed529b374dd017f072c7fa1df
https://doi.org/10.2514/1.50055
https://doi.org/10.2514/1.50055
Publikováno v:
AIAA Journal. 47:2359-2367
The combustion phenomena of doublet impingements of nitrogen tetroxide and monomethylhydrazine were observed in this research. The total flow rates of the propellants were controlled at 8:00 g=s to simulate the operation of a 5 lbf rocket, and the ra
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dcc0c803376c464f47ecde57fc3eb89e
https://doi.org/10.2514/1.41003
https://doi.org/10.2514/1.41003
Publikováno v:
51st AIAA/SAE/ASEE Joint Propulsion Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bc8d482909b2f87c6afabf09a430f616
https://doi.org/10.2514/6.2015-3847
https://doi.org/10.2514/6.2015-3847
Publikováno v:
51st AIAA/SAE/ASEE Joint Propulsion Conference.
Green (low toxicity) liquid rocket propellants have become attractive in recent years due to the features of the low cost and less environmental impact. However, the green propellants, such as kerosene/H2O2, usually have different operational conditi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::08236021116c9112708a29084dd7170d
https://doi.org/10.2514/6.2015-3765
https://doi.org/10.2514/6.2015-3765
Publikováno v:
AIAA Journal. 44:2259-2266
The spray phenomena of doublet and triplet impingements of nitrogen tetroxide (NTO) and monomethylhydrazine (MMH) simulants were studied by the planar laser induced fluorescence technique. The total flow rates of the simulants were controlled at ∼8
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::854fd6b0a91ffca8ddb4df89c2efe8fe
https://doi.org/10.2514/1.18375
https://doi.org/10.2514/1.18375
Publikováno v:
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
By the PLIF optical technique, this study focused on the development of the impinging type injector design of the 100-lbf level monomethylhydrazine/nitrogen tetroxide liquid rocket. The design of the multi-pair impinging injector plate is based on th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0026038486b6341109e722fb8b36b485
https://doi.org/10.2514/6.2012-3745
https://doi.org/10.2514/6.2012-3745
Publikováno v:
45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::92f7bcd75d00a1ae2a6620ca145bd42b
https://doi.org/10.2514/6.2009-4853
https://doi.org/10.2514/6.2009-4853