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특허 상세정보

Rocket cluster divert and attitude control system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-010/66    F42B-015/01    F42B-010/00    F42B-015/00   
출원번호 US-0258274 (2014-04-22)
등록번호 US-9377279 (2016-06-28)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Renner, Otto, Boisselle & Sklar, LLP
인용정보 피인용 횟수 : 0  인용 특허 : 17
초록

A flight vehicle includes a nose portion, a fuselage retaining structure aft of the nose portion, and an axial motor for expelling axial thrust along a longitudinal axis of the flight vehicle. Radial motors are coupled to the retaining structure and axisymmetrically arranged about the axial motor. Each radial motor is configured to expel radial thrust radially outwardly in respect to the flight vehicle. Roll thrusters are operatively coupled with the radial motors and coupled to the fuselage retaining structure. The roll thrusters are configured to provi...

대표
청구항

1. A flight vehicle comprising: a nose portion;a fuselage retaining structure aft of the nose portion;radial motors coupled to the fuselage retaining structure and arranged about a central longitudinal axis of the flight vehicle, each radial motor for expelling radial thrust and including a tank and a nozzle coupled to the tank for directing the radial thrust radially outwardly in respect to the flight vehicle;roll thrusters operatively coupled with the radial motors and coupled to the fuselage retaining structure, the roll thrusters for providing a roll...

이 특허에 인용된 특허 (17)

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  9. Carlson, Russell W.. Method and system for controlling solid propellant thrust. USP2013118584443.
  10. Chasman,Daniel B.; Leal,Michael; Haight,Stephen D.. Missile control system and method. USP2007107287725.
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