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  5. Maximum estimation of basic aircraft performance characteristics of a transport aerospace system

Maximum estimation of basic aircraft performance characteristics of a transport aerospace system

О.В. Solov'ev, E.A. Ukrainec, A.A. Shalygin, V.D. Komarov
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The estimation of maximal height and speed of flight of starting pilotless vehicle is conducted in composition a transport aerospace system. Composition of the aerospace system is certain, aerodynamic arrangement of the first stage is developed – starting pilotless vehicle.
Keywords: starting aircraft, aerospace system, aerodynamic arrangement, aircraft performance characteristics