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Spaceshuttle telescope-observatory

机译:航天飞机天文台

摘要

A Spaceshuttle telescope-observatory as a singular system has a circularly cross-sectioned long fuselage of a closed tipe and an opening nozzle-cone at the top of a secondary reflector that serves the primary reflector on the top side of the telescope-observatory, while the main reflector and the observatory is located at the bottom part of the fuselage, having the wings, each operative with turbable tips for the collecting of solar radiation. This system have to be launched conventionally by a large lifting body.
机译:作为一个单一系统的航天飞机望远镜天文台,其圆形横截面长的机身具有封闭的尖端,在次要反射镜的顶部具有一个开口的喷嘴锥,该副反射镜在望远镜天文台的顶部用作主反射镜,而主反射器和天文台位于机身底部,具有机翼,每个机翼均带有可旋转的尖端,用于收集太阳辐射。该系统通常必须由大的提升机构启动。

著录项

  • 公开/公告号US2003173465A1

    专利类型

  • 公开/公告日2003-09-18

    原文格式PDF

  • 申请/专利权人 HERPAY ZOLTAN;

    申请/专利号US20020100732

  • 发明设计人 ZOLTAN HERPAY;

    申请日2002-03-18

  • 分类号B64G1/22;B64G1/00;

  • 国家 US

  • 入库时间 2022-08-22 00:11:50

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