Geodesic
Ballistic design of interplanetary missions for the spacecraft with electrorocket propulsion
Matematičeskoe modelirovanie, Tome 12 (2000) no. 5, pp. 33-38.

Voir la notice de l'article provenant de la source Math-Net.Ru

The ballistic computations for the space missions' projects which purpose to use the space vehicles of the new generation are considered. The use of electrorocket propulsion will allow to reach some small bodies of the Solar System (asteroids, Mars saetellite Fobos, etc.) and to get the sample from them to the Earth. The goal of these missions is to get the new important data about creation of the Solar System. Contemporary methods of solving optimization problem and decomposition of the complex problem with analysis of plain model problems are used for ballistic design. 
@article{MM_2000_12_5_a4,
     author = {T. M. Eneev and R. Z. Akhmetshin and G. B. Efimov and M. C. Konstantinov and G. G. Fedotov},
     title = {Ballistic design of interplanetary missions for the spacecraft with electrorocket propulsion},
     journal = {Matemati\v{c}eskoe modelirovanie},
     pages = {33--38},
     publisher = {mathdoc},
     volume = {12},
     number = {5},
     year = {2000},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/MM_2000_12_5_a4/}
}
TY  - JOUR
AU  - T. M. Eneev
AU  - R. Z. Akhmetshin
AU  - G. B. Efimov
AU  - M. C. Konstantinov
AU  - G. G. Fedotov
TI  - Ballistic design of interplanetary missions for the spacecraft with electrorocket propulsion
JO  - Matematičeskoe modelirovanie
PY  - 2000
SP  - 33
EP  - 38
VL  - 12
IS  - 5
PB  - mathdoc
UR  - http://geodesic.mathdoc.fr/item/MM_2000_12_5_a4/
LA  - ru
ID  - MM_2000_12_5_a4
ER  - 
%0 Journal Article
%A T. M. Eneev
%A R. Z. Akhmetshin
%A G. B. Efimov
%A M. C. Konstantinov
%A G. G. Fedotov
%T Ballistic design of interplanetary missions for the spacecraft with electrorocket propulsion
%J Matematičeskoe modelirovanie
%D 2000
%P 33-38
%V 12
%N 5
%I mathdoc
%U http://geodesic.mathdoc.fr/item/MM_2000_12_5_a4/
%G ru
%F MM_2000_12_5_a4
T. M. Eneev; R. Z. Akhmetshin; G. B. Efimov; M. C. Konstantinov; G. G. Fedotov. Ballistic design of interplanetary missions for the spacecraft with electrorocket propulsion. Matematičeskoe modelirovanie, Tome 12 (2000) no. 5, pp. 33-38. http://geodesic.mathdoc.fr/item/MM_2000_12_5_a4/