发明名称 NOSE AERODYNAMIC FAIRING FOR SPACE VEHICLES WITH PARTS PROJECTING BEYOND THE MID-SECTION OF ROCKET BOOSTER
摘要 FIELD: space rocketry. ^ SUBSTANCE: each door of the nose aerodyanmic fairing is made of two sections with a cross joint. The plane of the joint coincides with the rear section of the fuselage fairing closed with cover in the mounted state. The cover is made in the form of a tapered surface integrated with the door section joined to the body of the rocket booster and rigidly connected to it in the point of conjugation. ^ EFFECT: enhanced operating and technical characteristics of the rocket booster. ^ 5 dwg
申请公布号 RU2245510(C1) 申请公布日期 2005.01.27
申请号 RU20030116550 申请日期 2003.06.03
申请人 发明人 ALLE A.JU.;BLINOV V.N.;BULYGIN JU.V.;GORLOV V.I.;IVANOV N.N.;KASATKIN G.M.;MARKELOV V.V.
分类号 F42B15/00 主分类号 F42B15/00
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