2,297
Views
107
CrossRef citations to date
0
Altmetric
Original Articles

A Model of AP/HTPB Composite Propellant Combustion in Rocket-Motor Environments

, &
Pages 2143-2169 | Published online: 21 Oct 2008

REFERENCES

  • Apte , S. and Yang , V. ( 2001 ) Unsteady flow evolution in a porous chamber with surface mass injection, I: Free oscillation . AIAA J. , 39 , 1577 – 1586 .
  • Apte , S. and Yang , V. ( 2002 ) Unsteady flow evolution and combustion dynamics of homogeneous solid propellant in a rocket motor . Combust. Flame , 131 , 110 – 131 .
  • Arisawa , H. and Brill , T.B. ( 1996 ) Flash pyrolysis of hydroxyl-terminated polybutadiene (HTPB) II: Implications of the kinetics to combustion of organic polymers . Combust. Flame , 106 , 131 – 143 .
  • Beck , W.H. ( 1987 ) Pyrolysis studies of polymeric materials used as binders in composite propellants: A review . Combust. Flame , 70 , 171 – 190 .
  • Beckstead , M.W. , Derr , R.L. , and Price , C.F. ( 1970 ) A Model of composite solid-propellant combustion based on multiple flames . AIAA J. , 8 , 2200 – 2207 .
  • Beddini , R.A. ( 1978 ) Reacting turbulent boundary-layer approach to solid propellant erosive burning . AIAA J. , 16 , 898 – 904 .
  • Bilger , R.W. , Jia , X. , Li , J.D. , and Nguyen , T.T. ( 1996 ) Theoretical and experimental study of composite solid propellant combustion . Combust. Sci. Technol. , 115 , 1 – 39 .
  • Brill , T.B. and Budenz , B.T. ( 2000 ) Flash pyrolysis of ammonia perchlorate-hydroxyl-terminated-polybutadiene mixtures including selected additives. In Yang , V. , Brill , T.B. , and Ren , W.Z. (Eds.) Solid Propellant Chemistry, Combustion and Motor Interior Ballistics, Progress in Astronautics and Aeronautics , AIAA , NY , Vol. 185 , 3 – 23 .
  • Buckmaster , J. , Jackson , T.L. , and Yao , J. ( 1999 ) An elementary discussion of propellant flame geometry . Combust. Flame , 117 , 541 – 552 .
  • Cai , W. ( 2001 ) Two-phase Flow Interactions and Combustion of AP/HTPB Composite Propellant in Rocket Motors with Acoustic Oscillations , Ph.D. Dissertation, Pennsylvania State University, University Park, PA .
  • Chaiken , R.F. and Anderson , W.H. ( 1960 ) The role of binder in composite propellant combustion . ARS Prog. Astro. Rocket , I , 227 – 249 .
  • Chen , J.K. and Brill , T.B. (1991) Chemistry and kinetics of hydroxyl-terminated polybutadiene (HTPB) and diisocyanate-HTPB polymers during slow decomposition and combustion-like conditions. Combust. Flame , 87, 217–232.
  • Chorpening , B.T. and Brewster , M.Q. ( 2002 ) Combustion behavior of AP/HTPB propellant sandwiches with Peclet and Damköhler number variations . Combust. Sci. Technol. , 174 ( 4 ), 39 – 60 .
  • Chu , W. and Yang , V. ( 1996 ) Combustion of AP-based composite propellant in a rocket motor flow environment . 32nd Joint Propulsion Conference, AIAA , 96 – 2885 .
  • Cohen , N.S. , Fleming , R.W. , and Derr , R.L. ( 1974 ) Role of binders in solid propellant combustion . AIAA J. , 12 , 212 – 218 .
  • Glick , R.L. ( 1974 ) On statistical analysis of composite solid propellant combustion . AIAA J. , 12 , 384 – 385 .
  • Godon , J.C. , Duterque , J. , and Lengelle , G. ( 1992 ) Solid propellant erosive burning . J. Propul. Power , 8 ( 4 ), 741 – 747 .
  • Gordon , S. and McBride , B.J. ( 1994 ) Computer program for calculation of complex chemical equilibrium compositions and applications . NASA Reference Publication 1311 .
  • Guirao , C. and Williams , F.A. ( 1971 ) A model for aluminum perchlorate deflagration between 20 and 100 atm . AIAA J. , 9 ( 7 ), 1345 – 1356 .
  • Hegab , A. , Jackson , T.L. , Buckmaster , J. , and Stewart , D.S. ( 2001 ) Nonsteady burning of periodic sandwich propellants with complete coupling between the solid and gas phases . Combust. Flame , 125 , 1055 – 1070 .
  • Hermance , C.E. ( 1960 ) A model of composite propellant combustion including surface heterogeneity and heat generation . AIAA J. , 4 , 1629 – 1637 .
  • Hsieh , S.Y. and Yang , V. ( 1997 ) A preconditioned flux-differencing scheme for chemically reacting flows at all Mach numbers . Int. J. Comp. Fluid Dyn. , 8 , 31 – 49 .
  • Ibiricu , M.M. and Williams , F.A. ( 1975 ) Influence of externally applied thermal radiation on the burning rates of homogeneous solid propellants . Combust. Flame , 24 , 185 – 198 .
  • Jackson , T.L. and Buckmaster , J. ( 2000 ) Nonpremixed periodic flames supported by heterogeneous propellants . J. Propuls. Power , 16 ( 3 ), 498 – 504 .
  • Jackson , T.L. and Buckmaster , J. ( 2002 ) Heterogeneous propellant combustion . AIAA J. , 40 ( 6 ), 1122 – 1130 .
  • Jacobs , P.W.M. and Whitehead , H.M. ( 1969 ) Decomposition and combustion of ammonium perchlorate . Chem. Rev. , 4 , 551 – 590 .
  • Jia , X. and Bilger , R.W. ( 1994 ) The Burke-Schumann diffusion flame with zero net flux boundary conditions . Combust. Sci. Technol. , 99 , 371 – 376 .
  • King , M.K. ( 1978 ) A model of erosive burning of composite propellants . J. Spacecraft , 15 ( 3 ), 139 – 146 .
  • King , M.K. ( 1981 ) Experimental and theoretical study of the effects of pressure and crossflow velocity on composite propellant burning rate . Proc. Combust. Instit. , 18 , 207 – 215 .
  • Kishore , K. ( 1979 ) Comprehensive view of the combustion models of composite solid propellants . AIAA J. , 17 , 1216 – 1224 .
  • Knott , G.M. and Brewster , M.Q. ( 2000 ) Two-dimensional combustion modeling of heterogeneous solid propellants with finite Peclet number . Combust. Flame , 121 , 91 – 106 .
  • Knott , G.M. and Brewster , M.Q. ( 2002 ) Modeling the combustion of propellant sandwiches . Combust. Sci. Technol. , 174 , 61 – 90 .
  • Knott , G.M. , Jackson , T.L. , and Buckmaster , J. ( 2001 ) Random packing of heterogeneous propellants . AIAA J. , 39 ( 4 ), 678 – 686 .
  • Lengelle , G. ( 1970 ) Thermal degradation kinetics and surface pyrolysis of vinyl polymers . AIAA J. , 8 ( 11 ), 1989 – 1998 .
  • Massa , L. , Jackson , T.L. , and Buckmaster , J. ( 2005 ) New kinetics for a model of heterogeneous propellant combustion . J. Propul. Power , 21 ( 5 ), 914 – 924 .
  • Nachbar , W. and Parks (1960) A Theoretical study of the burning of a solid propellant sandwich. ARS Prog. Astronaut. Rocketry , I, 207–226.
  • Oefelein , J.C. ( 1997 ) Simulation and Analysis of Turbulent Multiphase Combustion Processes at High Pressures . Ph.D. Dissertation, Pennsylvania State University .
  • Parr , T.P. and Hanson-Parr , D.M. ( 1996 ) Solid propellant diffusion flame structure . Proc. Combust. Instit. , 27 , 1981 – 1987 .
  • Prasad , K. and Price , E. W. ( 1992 ) A numerical study of the leading edge of laminar diffusion flames . Combust. Flame , 90 , 155 – 173 .
  • Price , E.W. ( 1995 ) Effect of multidimensional flamelets in composite propellant combustion . J. Propul. Power , 11 ( 4 ), 717 – 728 .
  • Price , E.W. , Sambamurthi , J.K. , Sigman , R.K. , and Panyam , R.R. ( 1986 ) Combustion of ammonium perchlorate-polymer sandwiches . Combust. Flame , 63 ( 3 ), 381 – 413 .
  • Radhakrishnan , T.S. and Rama Rao , M. ( 1981 ) Thermal decomposition pf ploybutadienes by pyrolysis gas chromatography . J. Polymer Sci. , 19 ( 12 ), 3197 – 3208 .
  • Ramakrishna , P.A. , Paul , P.J. , and Mukunda , H.S. ( 2002 ) Sandwich propellant combustion: Modeling and experimental comparison . Proc. Combust. Instit. , 29 , 2963 – 2973 .
  • Ramohalli , K.N.R. ( 1984 ) Steady-State burning of composite propellants under zero cross-flow situation . In Kuo , K.K. and Summerfield M. (Eds.) Fundamentals of Solid-Propellant Combustion, Progress in Astronautics and Aeronautics . AIAA , New York .
  • Razdan , M. and Kuo , K.K. ( 1982 ) Turbulent flow analysis of erosive burning of cylindrical composite solid propellants . AIAA J. , 20 ( 1 ), 122 – 127 .
  • Reid , R.C. , Prausnitz , J.M. , and Poling , B.E. ( 1987 ) The Properties of Gases and Liquids, , 4th ed., McGraw-Hill , New York .
  • Renie , J.P. and Osborn , J.R. ( 1983 ) Erosive burning . AIAA J. , 21 ( 12 ), 1681 – 1689 .
  • Roh , T.-S. , Tseng , I.-S. , and Yang , V. ( 1995 ) Effects of acoustic oscillations on flame dynamics of homogeneous propellants in rocket motors . J. Propul. Power , 11 ( 4 ), 640 – 650 .
  • Saderholm , C.A. ( 1964 ) A Characterization of erosive burning for composite H-series propellants . AIAA Solid Propellant Rocket Conference , Palo Alto , CA .
  • Seleznev , V.A. , Pokhil , P.F. , Maltsev , V.M. , and Bavykin , I.B. ( 1969 ) An optical method of measuring the burning surface temperature of condensed systems . Combust. Flame , 13 , 139 – 142 .
  • Shuen , J.S. , Liou , M.S. , and Leer , B.V. ( 1990 ) Inviscid flux-splitting algorithms for real gases with non-equilibrium chemistry . J. Comput. Phys. , 90 , 371 – 395 .
  • Summerfield , M. , Sutherland , G.S. , Webb , M.J. , Taback , H.J. , and Hall , K.P. ( 1960 ) The burning mechanism of ammonium perchlorate propellants . ARS Progress in Astronautics and Rocketry , I , 141 – 182 .
  • Tseng , L.S. and Yang , V. ( 1994 ) Combustion of a double-base homogeneous propellant in a rocket motor . Combust. Flame , 96 , 325 – 342 .
  • Waesche , R.H.W. and Wenograd , J. ( 1969 ) Calculation of solid propellant burning rate from condensed-phase decomposition kinetics . AIAA Paper , 69 – 145 .
  • Westbrook , C.D. and Dryer , F.L. ( 1981 ) Simplified reaction mechanisms for the oxidation of hydrocarbon fuels in flames . Combust. Sci. Technol. , 27 , 31 – 43 .
  • Zong , N. and Yang , V. ( 2007 ) An efficient preconditioning scheme for general fluid mixtures using primitive pressure-temperature variables . Int. J. Comp. Fluid Dyn. , 21 ( 5–6 ), 217 – 230 .

Reprints and Corporate Permissions

Please note: Selecting permissions does not provide access to the full text of the article, please see our help page How do I view content?

To request a reprint or corporate permissions for this article, please click on the relevant link below:

Academic Permissions

Please note: Selecting permissions does not provide access to the full text of the article, please see our help page How do I view content?

Obtain permissions instantly via Rightslink by clicking on the button below:

If you are unable to obtain permissions via Rightslink, please complete and submit this Permissions form. For more information, please visit our Permissions help page.