首页> 外国专利> Thruster-Solar-Sails or ThrusterRing-Spacecraft improved through additional fuel less steering/-attitude control ( - Attitude Control System - ACS ). Solar-Sail-Launch-System, consisting of a self expanding solar sail with docking station and primary fuel-less attitude control/-steering-system

Thruster-Solar-Sails or ThrusterRing-Spacecraft improved through additional fuel less steering/-attitude control ( - Attitude Control System - ACS ). Solar-Sail-Launch-System, consisting of a self expanding solar sail with docking station and primary fuel-less attitude control/-steering-system

机译：通过额外的无油转向/姿态控制（-姿态控制系统-ACS），改进了“推力太阳能帆”或“推力环航天器”。太阳能帆启动系统，包括一个带有扩展坞的自扩展太阳帆和无燃料的主姿态控制/转向系统

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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，以使质心和太阳辐射压力中心同时向彼此相反的方向移动;太阳能-帆-启动系统直接推出了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。

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公开/公告号US2008217482A1

专利类型
公开/公告日2008-09-11

原文格式PDF
申请/专利权人 FRANK ELLINGHAUS;
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申请/专利号US20060614081
发明设计人 FRANK ELLINGHAUS;
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申请日2006-12-21
分类号B64G1/40;
国家 US
入库时间 2022-08-21 20:16:49

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