首页> 外国专利> SPACECRAFT AND SPACECRAFT CARRIER OUTER PART INITIAL DESIGN DRAWING

SPACECRAFT AND SPACECRAFT CARRIER OUTER PART INITIAL DESIGN DRAWING

机译:航天器和航天器载体外部零件初始设计图

摘要

PURPOSE: To enable the safe, stable taking-off and landing of a spacecraft easily since the upper part of a spacecraft carrier is formed into a flat flying-off deck, and generate buoyancy easily at the time of taking-off since the lower part of the spacecraft and spacecraft carrier is formed into a flat outer deck. ;CONSTITUTION: The flying-off deck 20 and the outer deck 21 at the upper and lower part of a frame in spacecraft drawings 7, 8, 12, 15 and spacecraft carrier drawings 4, 5, 12, 15 are manufactured into flat decks on the whole by caulking duralumin plates or the like fixedly by rivets.;COPYRIGHT: (C)1994,JPO&Japio
机译:目的:为了使航天器的安全,稳定的起飞和着陆变得容易,因为航天器载体的上部形成了平坦的飞行甲板,并且在起飞时由于下部很容易产生浮力航天器和航天器载体的顶部形成平坦的外甲板。 ;组成:在航天器图7、8、12、15和航天器运载器图4、5、12、15中,框架上部和下部的飞行甲板20和外甲板21被制造成扁平甲板,整体:用铆钉固定硬铝板或类似物。;版权所有:(C)1994,日本特许厅和日本杂志

著录项

  • 公开/公告号JPH0692300A

    专利类型

  • 公开/公告日1994-04-05

    原文格式PDF

  • 申请/专利权人 KOYASU TAKAO;

    申请/专利号JP19920295486

  • 发明设计人 KOYASU TAKAO;

    申请日1992-09-14

  • 分类号B64G5/00;B64G1/60;

  • 国家 JP

  • 入库时间 2022-08-22 04:47:27

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