首页> 外国专利> Space transporter payload increasing system - uses container fitted into orbiting vehicle cargo hold and designed to allow independent re-entry and landing

Space transporter payload increasing system - uses container fitted into orbiting vehicle cargo hold and designed to allow independent re-entry and landing

机译:太空运输机有效载荷增加系统-使用安装在轨道车辆货舱中并设计为允许独立重新进入和着陆的集装箱

摘要

The payload of a space transporter is increased using a container which is capable of independently re-entering the atmosphere and landing. The container is fitted into part of the Orbiter cargo hold. The container is cylindrical, being 5.8 m long, 1.6 m in dia. and having convex ends. One end includes a heat shield (9) and braking rocket (11), an adjoining ring (12) housing control jets (13). In the other end is a parachute pack (10), electronic control (14) and communication (15) equipment such as a directional transmitter.
机译:使用能够独立重新进入大气层并着陆的容器来增加空间运输机的有效载荷。该容器已安装在Orbiter货舱的一部分中。该容器是圆柱形的,长5.8 m,直径1.6 m。并有凸出的末端。一端包括隔热罩(9)和制动火箭(11),一个装有控制喷嘴(13)的邻接环(12)。在另一端是降落伞包(10),电子控制装置(14)和通信装置(15),例如定向发射机。

著录项

  • 公开/公告号DE2716173A1

    专利类型

  • 公开/公告日1978-10-19

    原文格式PDF

  • 申请/专利权人 KLETTREINERDIPL.-ING.;

    申请/专利号DE19772716173

  • 发明设计人 KLETTREINERDIPL.-ING.;

    申请日1977-04-12

  • 分类号B64G1/00;

  • 国家 DE

  • 入库时间 2022-08-22 21:57:41

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