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High velocity impulse rocket

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-015/10   
미국특허분류(USC) 102/374 ; 60/253 ; 102/283 ; 102/347
출원번호 US-0013239 (1993-02-03)
발명자 / 주소
인용정보 피인용 횟수 : 16  인용 특허 : 0
초록
▼

An improved high energy impulse rocket includes a motor case containing propellant composed of individual, free flowing granules of a predetermined shape and unbonded to said motor case. The propellant has a high burning rate of 100 milliseconds or less and generates chamber pressures of up to about 50,000 psi. The rocket motor includes a reentry nozzle open at one end and connected to an exit nozzle, the reentry nozzle forming an annulus to contain the propellant and also forming a barrier to prevent ejection of the propellant during burning. Accelerati...

대표
청구항
▼

A high velocity impulse rocket, comprising: an outer rocket motor case, a reentry nozzle within said outer rocket motor case and forming an annulus therebetween, said reentry nozzle terminating in a discharge nozzle for exit of propulsion gases, a head member in said outer rocket motor case and spaced from said reentry nozzle, said reentry nozzle being in gas communication with said annulus whereby propulsion gases in said annulus flow in a first direction opposite said discharge nozzle, said head member and reentry nozzle being operative to cause the pr...

이 특허를 인용한 특허 피인용횟수: 16

  1. Tazzia Charles L. ; December Timothy S. ; Narayan Thirumurti. Cathodic electrocoat composition. USP2001046214470.
  2. Consaga John P.. Complexed liquid fuel compositions. USP2000086110306.
  3. Stewart William Brian ; Osment Donald Richard. Composite ply architecture for sabots. USP1998085789699.
  4. Riggs, Jeffrey L.; Oleynik, Vladislav; Borovikov, Valery; Albul, Gennadiy. Explosive decompression propulsion system. USP2012058181561.
  5. Vickery, Charles A.; Kruse, William D.; Olmos, Mark. External system and method for rocket exhaust plume signature tailoring. USP2003126655124.
  6. Olden, Thomas A.; Wrigglesworth, Walter. Flight vehicles including electrically-interconnective support structures and methods for the manufacture thereof. USP2014098826640.
  7. Schneider, Arthur J.. Guided kinetic penetrator. USP2010097795567.
  8. Olden, Thomas A.; Cavalleri, Robert J.. Modular divert and attitude control system. USP2012088242422.
  9. Cavalleri, Robert J.; Olden, Thomas A.. Pellet loaded attitude control rocket motor. USP2012038127534.
  10. Olden, Thomas A.; Cavalleri, Robert J.. Pellet-loaded multiple impulse rocket motor. USP2014038667776.
  11. Gould Robert L. (Westlake Village CA). Penetrating vehicle with rocket motor. USP1997015596166.
  12. Riggs, Jeffrey L.; Oleynik, Vladislav; Borovikov, Valery; Albul, Gennadiy. Projectile propulsion system. USP2012128327747.
  13. Vickery, Charles A.; Mason, Jerry N.; Kruse, William D.; Olmos, Mark. Rocket exhaust plume signature tailoring. USP2004026684622.
  14. Cavalleri, Robert J.; Olden, Thomas A.. Rocket motor with pellet and bulk solid propellants. USP2010037685940.
  15. Schmacker Bruce E.. Rocket-boosted guided hard target penetrator. USP2001086276277.
  16. Olden, Thomas A.; Wrigglesworth, Walter. Systems and methods for composite structures with embedded interconnects. USP2014088809689.

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