Measurement of Electron and Neutral Atom Density Downstream of an Electric Propulsion

Author(s):  
Naoji Yamamoto ◽  
Masataka Iwamoto ◽  
Taichi Morita ◽  
Hideki Nakashima
1989 ◽  
Vol 17 (5) ◽  
pp. 666-671 ◽  
Author(s):  
E. Hayess ◽  
B. Juttner ◽  
G. Lieder ◽  
W. Neumann ◽  
H. Pursch ◽  
...  

1982 ◽  
Vol 36 (2) ◽  
pp. 168-171 ◽  
Author(s):  
P. K. Schenck ◽  
J. C. Travis ◽  
G. C. Turk ◽  
T. C. O'Haver

The temporal and spatial evolution of the depleted neutral atom density following laser-enhanced ionization in laminar flow flames has been used to characterize the flow velocity of the flame gases. This technique utilizes a low power cw dye laser and a low sodium seed density (1011 to 1012 atoms/ml). The flow velocity can be measured to better than 2% in standard analytical burners.


Author(s):  
Ryo Kikuchi ◽  
Yuichi Hirano ◽  
Haruki Ejiri ◽  
Yuki Inada ◽  
Akiko Kumada ◽  
...  

1984 ◽  
Vol 75 ◽  
pp. 743-759 ◽  
Author(s):  
Kerry T. Nock

ABSTRACTA mission to rendezvous with the rings of Saturn is studied with regard to science rationale and instrumentation and engineering feasibility and design. Future detailedin situexploration of the rings of Saturn will require spacecraft systems with enormous propulsive capability. NASA is currently studying the critical technologies for just such a system, called Nuclear Electric Propulsion (NEP). Electric propulsion is the only technology which can effectively provide the required total impulse for this demanding mission. Furthermore, the power source must be nuclear because the solar energy reaching Saturn is only 1% of that at the Earth. An important aspect of this mission is the ability of the low thrust propulsion system to continuously boost the spacecraft above the ring plane as it spirals in toward Saturn, thus enabling scientific measurements of ring particles from only a few kilometers.


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