On the Space Thermal Destratification in a Partially Filled Hydrogen Propellant Tank by Jet Injection

2021 ◽  
Vol 34 (1) ◽  
Author(s):  
Ji-Cheng Li ◽  
Bin Guo ◽  
Jian-Fu Zhao ◽  
Kai Li ◽  
Wen-Rui Hu
1992 ◽  
Author(s):  
E. SCHOLZ ◽  
L. LOECHEL ◽  
M. ROBERTS

1999 ◽  
Author(s):  
Yoshiki Morino ◽  
Takashi Ishikawa ◽  
Takahira Aoki ◽  
Hisashi Kumazawa ◽  
Youichi Hayashi

2017 ◽  
Vol 749 (6) ◽  
pp. 19-23
Author(s):  
M.E. PILECKIJ ◽  
◽  
I.V. DIDRIKH ◽  
A.F. ZUBKOV ◽  
К.A. АNDRIANOV ◽  
...  

1996 ◽  
Author(s):  
Michael Debreceni ◽  
William Lay ◽  
T. Kuo ◽  
D. Jaekle, Jr.

npj Vaccines ◽  
2021 ◽  
Vol 6 (1) ◽  
Author(s):  
Rebecca L. Brocato ◽  
Steven A. Kwilas ◽  
Robert K. Kim ◽  
Xiankun Zeng ◽  
Lucia M. Principe ◽  
...  

AbstractA worldwide effort to counter the COVID-19 pandemic has resulted in hundreds of candidate vaccines moving through various stages of research and development, including several vaccines in phase 1, 2 and 3 clinical trials. A relatively small number of these vaccines have been evaluated in SARS-CoV-2 disease models, and fewer in a severe disease model. Here, a SARS-CoV-2 DNA targeting the spike protein and delivered by jet injection, nCoV-S(JET), elicited neutralizing antibodies in hamsters and was protective in both wild-type and transiently immunosuppressed hamster models. This study highlights the DNA vaccine, nCoV-S(JET), we developed has a great potential to move to next stage of preclinical studies, and it also demonstrates that the transiently-immunosuppressed Syrian hamsters, which recapitulate severe and prolonged COVID-19 disease, can be used for preclinical evaluation of the protective efficacy of spike-based COVID-19 vaccines.


2019 ◽  
Vol 1345 ◽  
pp. 032021
Author(s):  
T D Xin ◽  
D P Yang ◽  
Y S Duan

2014 ◽  
Vol 998-999 ◽  
pp. 613-616
Author(s):  
Li Li ◽  
Dong Ping Wang ◽  
Tsutomu Saito

The flow field was simulated in a 2D convergent-divergent nozzle, for fluidic thrust vectoring with N-S method. Based on the specific design, the effects of control parameters of secondary jet injection is investigated, and a method is proposed to calculate the initial state of secondary jet, which is different from original hypothesis of stagnation. The results showed that the two methods have closed results and the stagnation hypothesis is suitable for the calculation of the initial state of secondary jet.


Author(s):  
Bryan P. Ruddy ◽  
James W. Mckeage ◽  
Rhys M. J. Williams ◽  
Poul M. F. Nielsen ◽  
Andrew J. Taberner
Keyword(s):  

Sign in / Sign up

Export Citation Format

Share Document