[특허]Method and apparatus for disposal/recovery of orbiting space debris

Method and apparatus for disposal/recovery of orbiting space debris 원문보기

IPC분류정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	B64G-001/22 B64G-001/62
출원번호	US-0937057 (1992-08-26)
발명자 / 주소	Ting Paul C. (831 Fern Springs Ct. Houston TX 77062)
인용정보	피인용 횟수 : 34 인용 특허 : 0

초록 ▼

Method and apparatus for elimination of space debris from Earth orbit to thus minimize the hazards to space personnel and equipment that are now present as increasing as space exploration and use continues. As a first aspect space debris is collected and deorbited where it is completely burned by the heat developed by the kinetic energy of its reentry through the Earth\s atmosphere. As a second aspect, valuable space debris is collected and deorbited in a recovery reentry vehicle and which lands at a designated site on the Earth\s surface. A third method includes parking collected space debris in a designated parking orbit at a location well away from traveled orbit zones, including a high, relatively unused orbit sector. A fourth method includes solar and laser energy destruction of the non-valuable space debris while in orbit. A fifth aspect of this invention contemplates ejecting collected, containerized space debris from Earth orbit to an interplanetary orbit that does not intersect any planet of this solar system. The last method is to immediately remove the space debris after any new activities in space.

대표청구항 ▼

A method for disposal of orbiting space debris, comprising: (a) placing a space debris vehicle in orbit, said space debris vehicle having a space debris capture subsystem and a power subsystem in releasable assembly, said space debris capture subsystem having a receptacle for receiving space debris and dampers and damper control sensors for receiving said space debris within said receptacle; (b) placing in orbit a debris container of a dimension for containing a predetermined volume of space debris; (c) maneuvering said space debris vehicle by means of said power subsystem for collection of space debris within said receptacle of said space debris capture subsystem; (d) by manipulation of said space debris dampers by means of said damper control sensors transferring collected space debris from said space debris capture subsystem into said debris container; (e) decoupling said power subsystem from said space debris capture subsystem; coupling said debris container in powering and maneuvering assembly with said space debris vehicle (g) initiating deorbiting maneuvering of said debris container; for entry into the Earth\s atmosphere and for total destruction of said debris container and the space debris contained therein by means of heat developed by kinetic energy during entry into the Earth\s atmosphere; (h) decoupling said power subsystem from said debris container when predetermined deorbiting of said debris container is assured; and (i) reorbiting said power subsystem for further handling of space debris.

이 특허를 인용한 특허 (34)

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A62B-1/08	.. 윈치 또는 풀리에 제동기구가 있는 것

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Method and apparatus for disposal/recovery of orbiting space debris 원문보기

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Method and apparatus for disposal/recovery of orbiting space debris 원문보기

초록 ▼

대표청구항 ▼

연구과제 타임라인

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이 특허를 인용한 특허 (34)

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