发明名称 AIRCRAFT LAUNCH COMPLEX
摘要 FIELD: aeronautical engineering. SUBSTANCE: launch complex includes semi-fuselage carrier aircraft which has at least two fuselages located at some distance relative to each other, flying vehicle to be launched and supports intended for placing the vehicle to be launched. Supports for placing the above-mentioned vehicle on carrier aircraft are provided with guides which are located at the top relative to fuselages along their longitudinal axes. One support is provided with its own engine plants and rollers. EFFECT: improved aerodynamic characteristics. 4 cl, 4 dwg
申请公布号 RU2129508(C1) 申请公布日期 1999.04.27
申请号 RU19970100066 申请日期 1997.01.05
申请人 PETRAKOV VALERIJ MIKHAJLOVICH 发明人 PETRAKOV V.M.;KRUGLOV V.I.;KUZNETSOV V.A.;ZINCHENKO A.I.;GALJAEV V.I.
分类号 B64D5/00;B64C39/02;B64F1/04;(IPC1-7):B64D5/00 主分类号 B64D5/00
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