A Method for Express Analysis of Mechanical, Erosion, and Contaminating Impact of Plasma Jet of Electric Propulsion Thruster onto the Large Object of Space Debris

2019 ◽  
Vol 62 (4) ◽  
pp. 661-668
Author(s):  
S. S. Blyakharskii ◽  
Ya. S. Blyakharskii ◽  
A. B. Nadiradze ◽  
R. R. Rakhmatullin
2020 ◽  
Vol 43 (7) ◽  
pp. 1259-1268
Author(s):  
Mirko Leomanni ◽  
Gianni Bianchini ◽  
Andrea Garulli ◽  
Antonio Giannitrapani ◽  
Renato Quartullo

2010 ◽  
Vol 16 (5) ◽  
pp. 59-61
Author(s):  
N.M. Dron ◽  
◽  
L.G. Dubovik ◽  
A.I. Kondratyev ◽  
A.V. Khitko ◽  
...  

2015 ◽  
Vol 43 (12) ◽  
pp. 4200-4209 ◽  
Author(s):  
A. Ruggiero ◽  
P. Pergola ◽  
M. Andrenucci

2017 ◽  
Vol 55 (4) ◽  
pp. 270-274 ◽  
Author(s):  
A. A. Baranov ◽  
A. A. Budyanskiy ◽  
Yu. N. Razumnyi
Keyword(s):  

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.


1997 ◽  
Vol 7 (6) ◽  
pp. 1361-1375 ◽  
Author(s):  
O. H. Chang ◽  
A. Kaminska ◽  
M. Dudeck
Keyword(s):  

Sign in / Sign up

Export Citation Format

Share Document