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Aluminized plateau-burning solid propellant formulations and methods for their use

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) C06B-045/10   
미국특허분류(USC) 60/219 ; 149/019.4 ; 149/019.9 ; 149/019.92 ; 149/019.1
출원번호 US-0760727 (1996-12-05)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Cushman Darby & Cushman IP Group of Pillsbury Madison & Sutro, LLPLyons, Esq.
인용정보 피인용 횟수 : 8  인용 특허 : 24
초록
▼

Solid rocket motor propellants which burn at at least one stable burn rate over at least one corresponding pressure range (i.e the burn rate v. pressure curve contains at least one area of low pressure exponent with respect to a normal curve) are described. The propellant compositions comprise a binder, from about 65% to about 90% by weight ammonium perchlorate, the ammonium perchlorate being of at least two distinct particle sizes; from about 0.3% to about 5.0% by weight refractory oxide selected from the group consisting of TiO.sub.2, Al.sub.2 O.sub.3,...

대표
청구항
▼

[ What is claimed and desired to be secured by United States Letters Patent is:] [1.] A method for tailoring the performance of a metallized solid rocket motor propellant such that the propellant exhibits at least two stable burn rates over at least two corresponding pressure ranges comprising the steps of:incorporating within said propellant a biplateau burning amount of ammonium perchlorate having at least two distinct particle sizes, wherein a portion of the ammonium perchlorate particles have sizes in the range of from about 2.mu. to about 5.mu. and ...

이 특허에 인용된 특허 (24)

  1. Sayles David C. (Huntsville AL). A processing method for increasing propellant burning rate. USP1987044655860.
  2. Jacobs, Paul L.; Dunaway, J. C.. Active control of solid propellant generators using throat modulation techniques and programmable compensation. USP199002H000747.
  3. Ducote Marjorie E. (Huntsville AL) Allen Henry C. (Decatur AL). Amine salts as bonding agents. USP1985014493741.
  4. Sayles David C. (Huntsville AL). Burning rate enhancement of solid propellants by means of metal/oxidant agglomerates. USP1987044655858.
  5. Chi Minn-Shong (Newark DE). Composite propellants containing copper compounds as ballistic modifiers. USP1990114971640.
  6. McCulloch Charles R. (Shalimar FL) Moy Bertram K. (Shalimar FL). Composite propellants containing critical pressure increasing additives. USP1976103986910.
  7. Strecker Ruediger (Waldkraiburg DEX). Composite solid propellant. USP1989014798636.
  8. Graham ; William H. ; Shepard ; Inella G.. Control of cure rate of polyurethane resin based propellants. USP1978084110135.
  9. Graham William H. (Huntsville AL) Shepard Inella G. (Huntsville AL). Control of cure rate of polyurethane resins. USP1980014184031.
  10. Mori Atsuo (Hirakata JA) Kitamura Shuji (Toyonaka JA) Yamatsuta Kohji (Takatsuki JA). Curable urethane resin composition comprising a mixture of polyisocyanate, active hydrogen compound and diketo compound. USP1976083972846.
  11. Bolieau Christopher W. (Brigham City UT). Extendible wafer igniter with perforations adjacent the foot portion. USP1986034574699.
  12. Japs ; Archie B.. Gas generator and solid propellant with a silicon-oxygen compound as a burning rate modifier, and method for making the. USP1978074099376.
  13. Graham ; William Hardin ; Shepard ; Inella Gatlin. Hydroxy terminated polybutadiene based polyurethane bound propellant grains. USP1978074098626.
  14. Graham William H. (Huntsville AL) Shepard Inella G. (Huntsville AL). Hydroxy terminated polybutadiene based polyurethane bound propellant grains. USP1981044263444.
  15. Anderson William S. (Sunnyvale CA). Hydroxylic aromatic compounds as additives for rubber-based, composite solid propellants. USP1980014181545.
  16. White C. Max (Brigham City UT). Igniter for rocket motors. USP1985024498292.
  17. Duchesne Gonzague L. (Ste-Foy CAX) Perrault Guy (Ste-Foy CAX). Method of making a castable propellant. USP1985054517035.
  18. Herchin Michel A. (Saint Medard En Jalles FR) Blandin Jacques H. (Pontailler Sur Saone FR). Process for controlling the ballistic characteristics of double-base propellants. USP1976093979486.
  19. Strosser Richard P. (Akron PA) Wynn Edward J. (Leola PA) Chow Mark K. (Leola PA) Schlotterbeck Stephen C. (New Holland PA). Round baler with continuous bale size monitoring. USP1990054924405.
  20. Hightower ; James O. ; Hamner ; James W. ; Matthews ; Richard L.. Solid propellant with alumina burning rate catalyst. USP1978044084992.
  21. Ducote Marjorie E. (Huntsville AL). TMXDI, curing agent for hydroxy terminated propellant binders. USP1990044913753.
  22. Allen Henry C. (Decatur AL) Clarke Frederick W. (Huntsville AL). Tetra-alkyl titanates as bonding agents for thermoplastic propellants. USP1986074597924.
  23. Ecomard Andr (Marly le Roi FRX). Turbocharged internal combustion engine with a system for regulating the supercharged air pressure. USP1987044658587.
  24. Taylor ; Jr. Robert H. (Harvest AL). Use of controlled burn rate, reduced smoke, biplateau solid propellant formulations. USP1996125579634.

이 특허를 인용한 특허 피인용횟수: 8

  1. Hawkins David K. ; Campbell Carol J.. Advanced designs for high pressure, high performance solid propellant rocket motors. USP2000076086692.
  2. Anderson, Scott L.. Composite combustion catalyst and associated methods. USP2009127635461.
  3. Joe A. Martin ; Larry H. Welch. Composition and method for preparing oxidizer matrix containing dispersed metal particles. USP2002096454886.
  4. Villarreal, James K.; Deppert, Thomas M.; Langhenry, Mark T.; Summers, Matt H.. Electrically controlled variable force deployment airbag and inflation. USP2016109457761.
  5. Loehr, Richard D.; Villarreal, James K.. Electrically operated propellants with elevated self-sustaining threshold pressures. USP20190310220809.
  6. Campbell Carol Jean. Energetic oxetane propellants. USP2001046217682.
  7. Petersen, Eric L.; Seal, Sudipta; Stephens, Matthew; Reid, David L.; Carro, Rodolphe; Sammet, Thomas; Lepage, Alex. Solid propellant rocket motor having self-extinguishing propellant grain and systems therefrom. USP2012128336287.
  8. Martin, Joe A.; Welch, Larry H.. Variable burn-rate propellant. USP2003016503350.

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