Geodesic
The modeling of process of a space rocket landing from the plane-carrier
Matematičeskoe modelirovanie, Tome 18 (2006) no. 9, pp. 71-78 Cet article a éte moissonné depuis la source Math-Net.Ru

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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. 
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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/

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