首页> 外国专利> High-altitude launching of rockets lifted by helium devices and platforms with rotatable wings

High-altitude launching of rockets lifted by helium devices and platforms with rotatable wings

机译:带有可旋转机翼的氦气装置和平台可高空发射火箭

摘要

A system is disclosed for lifting a rocket into the upper atmosphere and establishing forward flight at several hundred miles per hour, before the rocket engines are ignited and the rocket is released from the lifting system. The main subassemblies of this lifting system comprise: (1) an array of large helium-filled dirigibles, of a size that can provide hundreds or thousands of tons of lifting force; (2) a tank-holding assembly that will be tethered to the dirigibles, and that will contain pumps and high-pressure tanks, to recapture and store the helium for use in subsequent launches; and, (3) a winged platform, with wings that can be rotated vertically during liftoff, and horizontally to establish forward flight after a desired altitude has been reached, and having conventional aircraft engines on each wing. This system enables safer, less expensive, and more efficient launching of rockets and heavy payloads into space, using easily reusable subassemblies.
机译:公开了一种系统,该系统用于在将火箭发动机点火并将火箭从举升系统释放之前,将火箭举升到高空并以每小时几百英里的速度建立向前飞行。该举升系统的主要组件包括:(1)一系列大型的氦填充飞轮,其尺寸可提供数百或数千吨的举升力; (2)一个罐子固定装置,该装置将被拴在飞船上,并装有泵和高压罐,以重新捕获和储存氦气,以便在随后的发射中使用; (3)一种机翼平台,其机翼在升空过程中可以垂直旋转,在达到所需高度后可以水平旋转以建立向前飞行,并且每个机翼上均具有常规的飞机发动机。该系统使用易于重复使用的子组件,可以更安全,更便宜,更高效地将火箭和重物发射到太空中。

著录项

  • 公开/公告号US2005116091A1

    专利类型

  • 公开/公告日2005-06-02

    原文格式PDF

  • 申请/专利权人 PATRICK D. KELLY;

    申请/专利号US20030692057

  • 发明设计人 PATRICK D. KELLY;

    申请日2003-10-23

  • 分类号B64B1/00;

  • 国家 US

  • 入库时间 2022-08-21 22:24:09

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