Geodesic
The modeling of process of a space rocket landing from the plane-carrier
Matematičeskoe modelirovanie, Tome 18 (2006) no. 9, pp. 71-78

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Dynamics of a space rocket exit process (landing) from a plane-carrier is simulated. The requirements to the schemes and means of landings are formulated, the application of a mathematical model for the absolute solids system is justified. Simulation results as dependence on time of absolute and relative motion space rocket and plane-carrier parameters and forces in the belts connection are presented. The results of calculation show a process realization possibility of principle. 
@article{MM_2006_18_9_a5,
     author = {S. V. Borzykh and D. V. Bakulin and Y. N. Shiblev and N. S. Ososov and A. V. Nikolaev},
     title = {The modeling of process of a space rocket landing from the plane-carrier},
     journal = {Matemati\v{c}eskoe modelirovanie},
     pages = {71--78},
     publisher = {mathdoc},
     volume = {18},
     number = {9},
     year = {2006},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/MM_2006_18_9_a5/}
}
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S. V. Borzykh; D. V. Bakulin; Y. N. Shiblev; N. S. Ososov; A. V. Nikolaev. The modeling of process of a space rocket landing from the plane-carrier. Matematičeskoe modelirovanie, Tome 18 (2006) no. 9, pp. 71-78. http://geodesic.mathdoc.fr/item/MM_2006_18_9_a5/