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Reduction gear of planetary exploration for atmospheric entry capsule

机译:大气进入舱的行星探测减速器

摘要

PURPOSE: To lessen weight and volume by lessening a mechanism for releasing a parachute. ;CONSTITUTION: While a capsule 1 is formed in the center of the body 2 with an air intake port 3 extending back and forth therethrough, a rear opening of the air intake port 3 is closed with a cap 7. When the capsule 1 re-enters the atmospher, the cap 7 is released from a restricting force by air pressure coming from the air intake port 3. Further, a parachute 6 is drawn out of the capsule 1 to be opened by the cap 7 releasing energy.;COPYRIGHT: (C)1993,JPO&Japio
机译:目的:通过减少释放降落伞的机制来减轻重量和体积。 ;构成:虽然胶囊1形成在主体2的中央,进气口3前后延伸,但进气口3的后部开口却用盖子7封闭。进入大气,通过来自进气口3的气压,帽7从约束力释放。此外,降落伞6从胶囊1中抽出,通过帽7释放能量而打开。 C)1993,日本特许厅

著录项

  • 公开/公告号JP2833299B2

    专利类型

  • 公开/公告日1998-12-09

    原文格式PDF

  • 申请/专利权人 NITSUSAN JIDOSHA KK;

    申请/专利号JP19910293529

  • 发明设计人 HONDA MASAHISA;

    申请日1991-11-11

  • 分类号B64G1/62;B64D17/62;

  • 国家 JP

  • 入库时间 2022-08-22 02:28:32

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