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REUSABLE MISSILE AND AIRCRAFT UNIT AND WAY TO RETURN IT TO SPACEPORT

机译:可重复使用的导弹和飞机装置以及将其返回太空的方法

摘要

FIELD: space-rocket equipment.; SUBSTANCE: invention refers to the field of space-rocket equipment and relates to aerodynamic configurations and ways of returning of the reusable missile and aircraft units (RMAU) to the spaceport. These units act as rocket boosters forming the first step of the mother missile (MM) while coupling its bodies (1) with the second step (18) of the MM. The housing (1) of the RMAU has a typical tandem configuration of the tanks and the liquid fuel sustainers (LFS). The unswept wing with folded lips in the start configuration is situated along the housing (1). After the RMAU has been separated from the second step (18), this wing rotates to the working position athwart the housing roll axis. The tail group protrudes to the working position from the tapered module (17) that is opposite to the LFS module. The outstanding nozzles of the liquid fuel sustainer are covered with the cowling that consists of movable protection flaps (3). Thus transformation of the RMAU into a sailplane is completed. Its flight to the landing aerodrome (with the LFS module at the front) is performed with the help of the sliding (14) (or dismountable) air-breathing engines.; EFFECT: increase of the payload weight part in the initial mass of the MM and reduction of resource consumption when the RMAU returns to the spaceport.;13 cl, 16 dwg
机译: FIELD:太空火箭装备。 物质:本发明涉及太空火箭装备领域,并且涉及空气动力学结构以及将可重复使用的导弹和飞行器单元(RMAU)返回空间端口的方式。这些单元充当火箭助推器,形成母导弹(MM)的第一步,同时将其主体(1)与MM的第二步(18)耦合。 RMAU的外壳(1)具有油箱和液体燃料保持器(LFS)的典型串联配置。处于起步状态的未折叠机翼带有折叠的唇缘,沿着机壳(1)放置。在RMAU与第二步(18)分离之后,该机翼旋转到不打滑外壳滚动轴的工作位置。尾部组从与LFS模块相对的锥形模块(17)突出到工作位置。液体燃料保持器的突出喷嘴被整流罩覆盖,该整流罩由可移动的保护翼片(3)组成。这样就完成了将RMAU转换为滑翔机的工作。滑行式(14)(或可拆卸)呼吸引擎帮助飞机飞到着陆机场(前排LFS模块)。 效果:当RMAU返回空间端口时,MM初始质量中有效载荷重量部分增加,资源消耗减少。; 13 cl,16 dwg

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