发明名称 MULTI-MODE AIRCRAFT-BOOSTER FOR AVIATION ROCKET SPACE COMPLEX
摘要 aeronautical and space engineering; space complexes for injection of space objects into orbits. SUBSTANCE: according to invention, supersonic aircraft of integral configuration at smooth conjugation of fuselage and variable-geometry wing; it is provided with all- moving vertical and horizontal tails and power-plant pods. Proposed booster aircraft is made for carrying launch vehicle (having mass of about 50 tons) under fuselage between power-plant pods. Compartment of fuselage may be used for receiving smaller launch vehicle (having masses lesser than 40 tons). Booster aircraft is provided with equipment for performing functions of aircraft command measuring point Booster aircraft may be used for launching rocket (rockets) at supersonic or subsonic speed followed by shifting to mode set by command and measuring point. Provision is made for wide selection of geographic of launch (inclination of orbits) and in-flight refueling. EFFECT: low cost of injection of payload; enhanced adaptability of space rocket complex. 2 cl, 3 dwg
申请公布号 RU2175934(C2) 申请公布日期 2001.11.20
申请号 RU19990122780 申请日期 1999.10.28
申请人 OBSHCHESTVO S OGRANICHENNOJ OTVETSTVENNOST'JU "TEK 发明人 BLIZNJUK V.I.;ALESHIN E.A.;BENDEROV V.V.;BONDARENKO N.N.;KLIMENKO V.I.;ROSTOPCHIN V.V.;CHEVARDOV S.G.
分类号 B64G1/00;B64G1/14 主分类号 B64G1/00
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