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특허 상세정보

Rocket propelled payload with divert control system within nose cone

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-010/60    F42B-015/01    F42B-010/66    F42B-010/00    F42B-015/00   
미국특허분류(USC) 244/003.22; 244/001R; 244/003.1; 244/003.15; 244/003.21; 244/117R; 244/119; 244/121; 244/158.1; 244/171.7; 244/173.1; 343/872; 102/374; 102/377
출원번호 US-0669935 (2012-11-06)
등록번호 US-9018572 (2015-04-28)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Cantor Colburn LLP
인용정보 피인용 횟수 : 0  인용 특허 : 21
초록

A rocket is provided and includes booster stages at a rear of the nose cone, the booster stages being configured for propelling the nose cone in a propulsion direction and a divert control system housed entirely in the nose cone for controlling an orientation of the propulsion direction.

대표
청구항

1. A rocket, comprising: a nose cone including a payload having a payload attitude control system (ACS);booster stages sequentially disposed at a rear of the nose cone, the booster stages being configured for propelling the nose cone in a propulsion direction; anda divert control system housed entirely in the nose cone for controlling an orientation of the propulsion direction, wherein:the nose cone is configured for ejection from the booster stages once a predefined velocity is attained, andthe payload is configured for ejection from the nose cone follo...

이 특허에 인용된 특허 (21)

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