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Solar sail launch system and solar sail attitude control system

机译:太阳帆发射系统和太阳帆姿态控制系统

摘要

Fuel less ACS for solar sails, using furl- and unfurl able ballast-sail-foil-segments for simultaneously displacement of center of mass and center of solar radiation pressure into opposite directions to each other.;Solar-Sail-Launch-System for direct launch of the System-Sail including already docked in daughter units and payload in the sailcraft's central docking station.;Unlike todays launch able solar sail designs the System-Sail features ample solar cell arrays and additional SEP-thruster-units for steering and propulsion, while the solar sail rather serves for longtime fuel less attitude controls and station keeping.;The SEP-Sailcraft may also serve as a carrier-ship for daughter-units in asteroid exploration missions and is able to deliver prospector landers back to LEO with furled in foils.
机译:用于太阳帆的无燃料ACS,使用可卷曲和不卷曲的压舱-帆-箔节段,使质心和太阳辐射压力中心同时向彼此相反的方向移动。推出了System-Sail,包括已经停靠在帆艇中央停靠站中的子单元和有效载荷;与今天的发射型太阳帆不同,System-Sail设计有充足的太阳能电池阵列以及用于转向和推进的附加SEP推进器单元, SEP-Sailcraft还可作为小行星探索任务中的子机的运输船,并能够将探空着陆器收起并返回LEO。箔纸。

著录项

  • 公开/公告号US7913953B2

    专利类型

  • 公开/公告日2011-03-29

    原文格式PDF

  • 申请/专利权人 FRANK WERNER ELLINGHAUS;

    申请/专利号US20060614081

  • 发明设计人 FRANK WERNER ELLINGHAUS;

    申请日2006-12-21

  • 分类号B64C1/10;

  • 国家 US

  • 入库时间 2022-08-21 18:08:23

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