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특허 상세정보

Spacecraft angular momentum stabilization system and method

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64G-001/10    B64G-001/28   
미국특허분류(USC) 244/158R ; 244/165
출원번호 US-0485294 (1983-04-15)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 14  인용 특허 : 3
초록

An improved system and method of ejecting a spacecraft from a shuttle or orbiter type craft in space includes a momentum wheel on the spacecraft that has a spin axis parallel to the ejection direction, spinning-up this momentum wheel prior to ejection and after ejection de-spinning this wheel whereby the whole spacecraft spins without the need of a spin table on the shuttle or orbiter craft.

대표
청구항

A method for placing a spacecraft in orbit from the cargo bay of the space shuttle or orbiter type craft where the satellite is mounted in an ejection direction perpendicular to the longitudinal axis of the shuttle craft and where said spacecraft and a perigee motor are fixed to each other to form a spacecraft/perigee motor assembly comprising the steps of: providing said spacecraft from a momentum wheel that has a spin axis in the launch direction; spinning said momentum wheel so that the momentum vector is parallel to the ejection direction of the spac...

이 특허를 인용한 특허 피인용횟수: 14

  1. Belbruno Edward A.. Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same. USP2001066253124.
  2. Belbruno Edward A.. Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same. USP2000086097997.
  3. Belbruno, Edward A.. Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same. USP2004066751531.
  4. Belbruno, Edward A.. Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same. USP2003066577930.
  5. Belbruno,Edward A.. Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same. USP2006026999860.
  6. Edward A. Belbruno. Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same. USP2002016341250.
  7. Peck,Mason A.. Momentum stabilized launch vehicle upper stage. USP2006087090171.
  8. Barnett Clifford J. (Costa Mesa CA) Greenwood John E. (Anaheim CA) Holman Earl V. (Whittier CA). Payload deployment method and system. USP1989084860974.
  9. Edward A. Belbruno. Procedure for generating operational ballistic capture transfer using a computer implemented process. USP2002086442482.
  10. Belbruno Edward A.. Procedure for generating operational ballistic capture transfer using computer implemented process. USP2001086278946.
  11. Fowell Richard A. (Culver City CA) Yocum John F. (Rancho Palos Verdes CA). Satellite spin axis stabilization using a single degree of freedom transverse momentum storage device. USP1997095667171.
  12. Fowell Richard A.. Satellite spin inversion using a single degree of freedom momentum storage device. USP1998065758846.
  13. Richard A. Fowell. Satellite spin reorientation using a single degree of freedom momentum storage device. USP2002056382565.
  14. Edward A. Belbruno. System and method of a ballistic capture transfer to L4, L5. USP2002056385512.