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Energy efficient solid propellant attitude control system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64G-001/26    B64G-001/42   
미국특허분류(USC) 244/169 ; 290/52 ; 60/3907 ; 60/3933
출원번호 US-0927290 (1986-11-04)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 9  인용 특허 : 3
초록
▼

An energy efficient solid propellant attitude control system for use on post boost vehicles equipped with post boost control systems, post boost propulsion systems, and velocity control systems utilizes gas from a gas generator to drive a gas turbine which drives an alternator to produce electrical power. The turbine effluent gas is selectively directed to highly vectorable hinged nozzles to provide attitude control for the post boost vehicle. Power from the alternator is used to drive electromechanical actuators which orient the highly vectorable hinged...

대표
청구항
▼

An energy efficient solid propellant attitude control system for a post boost space vehicle having an aft end comprising, a solid propellant gas generator for generating a flow of generated gas, a plurality of nozzles mounted on the aft end of the post boost space vehicle for providing attitude control of the post boost space vehicle, means directing said flow of generated gas through said nozzles to the environment to control the attitude of the post boost space vehicle, said nozzles being highly vectorable hinged nozzles having a side gas inlet through...

이 특허에 인용된 특허 (3)

  1. Frosch Robert A. (Administrator of the National Aeronautics and Space Administration with respect to an invention of Newport News VA 23602) Lawing Pierce L. (88 Columbia Dr. Newport News VA 23602) Pa. Cooling system for high speed aircraft. USP1981064273304.
  2. Douglass, Randle; Jacquin, H. George; Chewey, Paul M.; Galvan, Paul A.; Naragon, Richard S.. Dual pressure solid propellant control system. USP1985114550888.
  3. Muenger James R. (Beacon NY) Barber Everett M. (Wappingers Falls NY). Process for the generation of power from carbonaceous fuels with minimal atmospheric pollution. USP1980034193259.

이 특허를 인용한 특허 피인용횟수: 9

  1. Fujita, Toshiharu; Hayakawa, Nobuaki. Orbit attitude control device, and method of controlling orbit attitude. USP2016019242745.
  2. Fujita, Toshiharu; Hayakawa, Nobuaki. Orbit attitude control device, and method of controlling orbit attitude. USP2016109469419.
  3. Fujita, Toshiharu; Hayakawa, Nobuaki. Orbit attitude control device, and method of controlling orbit attitude. USP2017079696726.
  4. Fujita, Toshiharu; Hayakawa, Nobuaki. Orbit attitude control device, and method of controlling orbit attitude. USP2016049302790.
  5. Fujita, Toshiharu; Hayakawa, Nobuaki. Orbit attitude control device, and method of controlling orbit attitude. USP2016069365300.
  6. Quartararo Richard. Spacecraft attitude control with gimbaled thrusters. USP2000086102337.
  7. Abernethy David K.. Spacecraft sun-target steering about an arbitrary body axis. USP1999085934620.
  8. Bernard M. Anzel. Thruster systems for spacecraft station changing, station keeping and momentum dumping. USP2002086435457.
  9. Hill, David G.. Turbine powered electromechanical actuation system. USP2014058727284.

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