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SPACE VEHICLE FOR DESCENT IN ATMOSPHERE OF PLANET AND METHOD OF DESCENT OF SPACE VEHICLE IN ATMOSPHERE OF PLANET

机译:行星大气中的降体空间车辆和行星大气中的空间降体方法

摘要

FIELD: rocketry and space engineering. SUBSTANCE: space vehicle has heat-insulated load-bearing case with blunted nose portion, bottom shield, gas-dynamic flight control devices for control of flight at atmospheric section of trajectory, payload unit and landing complex. Case consists of upper and lower parts directed to flow and provided with shield; case is provided with aft flap; lower part of case and flap are made in form of members of spherical segment engageable with blunted nose part of vehicle; bottom shield is also spherical; split flap is articulated for control of vehicle by pitching and rolling channels. Descent of space vehicle includes orientation and braking of vehicle before atmosphere entry, stabilization of it in atmosphere by pitching, yawing and rolling channels and placing landing devices in operation. At speeds ranging from hypersonic to supersonic, flap is deflected in pitching and rolling plane through programmed angles at simultaneous stabilization of space vehicle at trimming angle of attack by means of gas-dynamic control devices. Invention makes it possible to perform manoeuvre of space vehicle having mass of up to 15 tons through lateral range of up to 1000 km. Maximum probable packaging density of interior volume with payload is retained at this. EFFECT: enhanced reliability. 3 cl, 7 dwg
机译:领域:火箭和太空工程。物质:航天器具有隔热的承重箱,其机头部分钝化,底部护罩,气动飞行控制装置,用于控制轨迹的大气部分,有效载荷单元和着陆区的飞行。箱体由上下两部分组成,上下部分均设有防护罩。箱子装有后挡板;壳体和襟翼的下部制成球形部分的形式,可与车辆的钝头部分接合。底罩也是球形的;铰接式分离翻板可通过俯仰和滚动通道来控制车辆。航天器的下降包括在大气进入之前对车辆进行定向和制动,通过俯仰,偏航和滚动通道使其稳定在大气中以及使着陆装置处于运行状态。在从高超音速到超音速的速度范围内,襟翼通过气动力控制装置在俯仰和滚动平面上通过编程角度偏转,同时使航天器稳定在微调迎角。本发明使得可以在最大1000公里的侧向范围内执行质量最大为15吨的航天器的操纵。保持带有有效载荷的内部容积的最大可能包装密度。效果:增强的可靠性。 3厘升,7载重吨

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