The modeling of process of a space rocket landing from the plane-carrier

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.