发明名称 АВИАЦИОННЫЙ РАКЕТНЫЙ КОМПЛЕКС
摘要 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
申请公布号 RU2005133938(A) 申请公布日期 2007.05.10
申请号 RU20050133938 申请日期 2005.11.02
申请人 Федеральное государственное унитарное предпри тие"Государственный ракетный центр "КБ им. акад. В.П. Макеева" (RU) 发明人 Данилкин В чеслав Андреевич (RU);Дегт рь Владимир Григорьевич (RU);Сабуренко Валерий Васильевич (RU);Шевалдина Лариса Витальевна (RU);Карпов Анатолий Степанович (RU)
分类号 B64G1/14 主分类号 B64G1/14
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