发明名称 АВИАЦИОННЫЙ РАКЕТНЫЙ КОМПЛЕКС
摘要 FIELD: transport. ^ SUBSTANCE: aviation rocket-launching complex includes airplane, carrier rocket of airborne launching, systems securing their functioning, transport-take-off platform and cable-halyard. Carrier rocket is equipped with wing, head and tail cowlings with stabiliser and vertical empennage installed. Wing variable sweep after take-off is foreseen. Cable-halyard is connected with wing centre-section and airplane is functioning as towplane for carrier rocket. ^ EFFECT: increase of admissible dimensions and launching mass of carrier rocket and spacecrafts launched to orbit. ^ 1 dwg
申请公布号 RU2005134824(A) 申请公布日期 2007.05.20
申请号 RU20050134824 申请日期 2005.11.09
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)
分类号 B64G1/00 主分类号 B64G1/00
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