FIELD: aviation.
SUBSTANCE: invention is related to the field of aviation rocket-space engineering. Aviation rocket complex comprises airplane, carrier rocket for air starting and systems that provide for their functioning. Besides aviation rocket complex comprises glider equipped with carrier rocket, transport-overspeed platform, on which glider is installed, towing rope-halyard that couples glider and airplane. Glider wing is arranged as variable in area. Separate bearing parts are fixed to central wing section that are equivalent pairwise and installed symmetrically on wing ends. Mentioned parts are connected to each other with the possibility of their separation in flight by command from control system, for instance with application of detonating extended charges installed along perimetres of profiles of separating wing bearing parts.
EFFECT: invention is aimed at increase of carrier rocket dimensions and starting weight and therefore weights of spacecrafts put in orbit are increased.
1 dwg
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Authors
Dates
2009-06-27—Published
2005-11-02—Filed