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특허 상세정보

Controlled autoignition propellant systems

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-009/95    F02K-009/12    F02K-009/14    F02K-009/08    F02K-009/28    C06B-045/10   
출원번호 US-0200597 (2002-07-23)
등록번호 US-9759162 (2017-09-12)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Nixon & Vanderhye, P.C.
인용정보 피인용 횟수 : 0  인용 특허 : 19

Solid propellant systems include a main propellant and a secondary propellant in contact with the first propellant that exhibits autoignition temperatures of at least about 100° F. lower than the autoignition temperature of the main propellant. The secondary propellant of the present invention is most advantageously employed with conventional AP-containing solid propellant formulations as the main propellant, especially formulations containing both AP, an energetic solid, and a binder. In especially preferred forms, the secondary propellant will include ...


1. A solid rocket motor propellant system comprising: (a) an ammonium perchlorate-based main propellant which comprises, based on the total weight of the main propellant, between about 65 to about 92 wt. % ammonium perchlorate (AP), between about 8 to about 25 wt. % of an inert binder, and optionally, between about 5 to about 20 wt. % of aluminum powder; and(b) a secondary propellant in the form of a strip in localized contact with said main propellant of a compressed mass of a composition which comprises, based on the total weight of the secondary prope...

이 특허에 인용된 특허 (19)

  1. Scheffee Robert S.. Autoignition system for inflator devices with separator that melts. USP2000056062142.
  2. Smith John R. (Kettering OH). Combined cycle ramjet engine. USP1984044441312.
  3. Wheatley Brian K.. Gas generating composition with exploded aluminum powder. USP1999085936195.
  4. Ryder David D.. Gas generating material for vehicle occupant protection device. USP2000116143103.
  5. Scheffee Robert S. ; Wheatley Brian K.. Gas-generative composition consisting essentially of ammonium perchlorate plus a chlorine scavenger and an organic fuel. USP1999015861571.
  6. Knowlton Gregory D. ; Anderson Bruce B. ; Gortemoller Theodore B.. Heat transfer delay. USP2001106298784.
  7. Hamilton Brian K. ; Parks Brent A.. Hybrid inflator with coaxial chamber. USP1998015711546.
  8. Nixon Robert J.,GBX ; Lewin Martin J.,GB2 ; Spellward Terence L.,GBX. Long range artillery shell. USP1999035886289.
  9. Hutchens Dale E. ; Cohen Norman. Low smoke rocket motor liner compositions. USP2000046051087.
  10. Reed ; Jr. Russell (Ridgecrest CA) Price Raymond M. (Ridgecrest CA). Method of making a gun propellant composition. USP1981084283237.
  11. Marguet Roger (Issy les Moulineaux FRX) Petit Bernard (Les Ulis Bures FRX) Naduad Lionel (Massy FRX) Borton Pierre (Boulogne Billancourt FRX). Power units of the ram-jet engine type. USP1996075537815.
  12. Ducote Marjorie E. (Huntsville AL). Prevention of unwanted cure catalysis in isocyanate cured binders. USP1986074597811.
  13. Haaland Andrew C. ; Braithwaite Paul C. ; Hartwell James A. ; Lott Val D. ; Rose Michael T.. Process for the manufacture of high performance gun propellants. USP1998065759458.
  14. Kassuelke Gregory T. ; Candland Calvin T. ; Kennedy James L.. Propellant system. USP1998015712445.
  15. Schedlbauer Fritz (Pfinztal DEX). Pyrotechnic charge for releasing enclosed pressurized gas. USP1997045623121.
  16. Younkin Harry A. (Newark DE). Radial end burner rocket motor. USP1979044148187.
  17. Grosgebauer Roger A. (Ogden UT) White C. Max (Brigham City UT). Radial pulse motor igniter-sustain grain. USP1991034999997.
  18. Nagy Joseph G. (St. Louis County MO) Jaspering Daniel L. (St. Charles MO). Solid fuel burn enhancer. USP1990014891938.
  19. Hightower ; Jr. James O. (Huntsville AL) Sato Tomio (Huntsville AL). Solid rocket motor propellants with reticulated structures embedded therein to provide variable burn rate characteristic. USP1988074756251.