$\require{mediawiki-texvc}$

연합인증

연합인증 가입 기관의 연구자들은 소속기관의 인증정보(ID와 암호)를 이용해 다른 대학, 연구기관, 서비스 공급자의 다양한 온라인 자원과 연구 데이터를 이용할 수 있습니다.

이는 여행자가 자국에서 발행 받은 여권으로 세계 각국을 자유롭게 여행할 수 있는 것과 같습니다.

연합인증으로 이용이 가능한 서비스는 NTIS, DataON, Edison, Kafe, Webinar 등이 있습니다.

한번의 인증절차만으로 연합인증 가입 서비스에 추가 로그인 없이 이용이 가능합니다.

다만, 연합인증을 위해서는 최초 1회만 인증 절차가 필요합니다. (회원이 아닐 경우 회원 가입이 필요합니다.)

연합인증 절차는 다음과 같습니다.

최초이용시에는
ScienceON에 로그인 → 연합인증 서비스 접속 → 로그인 (본인 확인 또는 회원가입) → 서비스 이용

그 이후에는
ScienceON 로그인 → 연합인증 서비스 접속 → 서비스 이용

연합인증을 활용하시면 KISTI가 제공하는 다양한 서비스를 편리하게 이용하실 수 있습니다.

Method for injecting payloads into orbit 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64G-001/24
출원번호 US-0111095 (1993-08-24)
발명자 / 주소
  • Frazier Scott R. (Herndon VA)
출원인 / 주소
  • Orbital Sciences Corporation (Dulles VA 02)
인용정보 피인용 횟수 : 24  인용 특허 : 0

초록

The present invention comprises a method for injecting a heavier payload into orbit than is possible using a traditional method and the same rocket booster launch vehicle. The method of the present invention does not utilize a parking orbit and does not perform orbital injection at perigee or apogee

대표청구항

A method for injecting a payload into an elliptical orbit having its line of apsides at a specific initial location comprising the steps of: firing at least one lower stage engine of a rocket booster vehicle carrying the payload so as to launch the rocket booster vehicle and payload along a suborbit

이 특허를 인용한 특허 (24)

  1. Healy, Liam M., Control system and method for a plane change for satellite operations.
  2. Salkeld, Robert, Direct flight far space shuttle.
  3. Post, Kevin E.; Belbruno, Edward, Fast-low energy transfer to Earth-Moon Lagrange point L2.
  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.
  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.
  6. Belbruno, Edward A., Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same.
  7. Belbruno, Edward A., Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same.
  8. Belbruno,Edward A., Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same.
  9. Edward A. Belbruno, Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same.
  10. Koppel Christophe,FRX ; Valentian Dominique,FRX, Method and a system for launching satellites on non-coplanar orbits, making the use of gravitational assistance from the moon.
  11. Koppel Christophe,FRX ; Valentian Dominique,FRX, Method and a system for launching satellites simultaneously on non-coplanar orbits by using highly eccentric orbits and.
  12. Koppel Christophe,FRX, Method and a system for putting a space vehicle into orbit, using thrusters of high specific impulse.
  13. Koppel Christophe,FRX, Method and a system for putting a space vehicle into orbit, using thrusters of high specific impulse.
  14. Rockwell Donald, Method for satellite injection using a solid fuel rocket motor.
  15. Hache, Raphaël; Kaltenbach, Alexandre; Tessandori, Stéphane, Method for stationing a satellite and in-orbit testing of its payload.
  16. Rosen, Harold A., Molniya orbit satellite systems, apparatus, and methods.
  17. Gelon,Walter; Kamel,Ahmed; Stratemeier,Darren; Hur Diaz,Sun, Practical orbit raising system and method for geosynchronous satellites.
  18. Edward A. Belbruno, Procedure for generating operational ballistic capture transfer using a computer implemented process.
  19. Belbruno Edward A., Procedure for generating operational ballistic capture transfer using computer implemented process.
  20. Salkeld, Robert, Reusable global launcher.
  21. Caplin, Glenn N.; Rosen, Harold A.; Fowler, Harmon C., Satellites and satellite fleet implementation methods and apparatus.
  22. Caplin, Glenn N.; Rosen, Harold A.; Fowler, Harmon C., Satellites and satellite fleet implementation methods and apparatus.
  23. Healy, Liam M., System and method for maneuver plan for satellites flying in proximity using apocentral coordinate system.
  24. Edward A. Belbruno, System and method of a ballistic capture transfer to L4, L5.
섹션별 컨텐츠 바로가기

AI-Helper ※ AI-Helper는 오픈소스 모델을 사용합니다.

AI-Helper 아이콘
AI-Helper
안녕하세요, AI-Helper입니다. 좌측 "선택된 텍스트"에서 텍스트를 선택하여 요약, 번역, 용어설명을 실행하세요.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.

선택된 텍스트

맨위로