Non-Steady Combustion of Composite Propellants Subjected to Rapid Depressurization

REFERENCES

• et al. ( 1973 ). Measurement of steady state and transient solid propellant burning rates with microwaves . Georgia Institute of Technology , Atlanta , Final Report Grant AFOSR-70-1934 .
   Google Scholar
• et al. ( 1970 ). A model for composite solid propellant combustion based on multiple flames . AIAA J. , 8 ( 12 ), 2200 .
   Google Scholar
• et al. . ( 1968 ). Surface reaction effects on the acoustic response of composite solid propellants . AIAA J. , 6 ( 3 ), 479 .
   Google Scholar
• Culick , F. E. C. ( 1968 ). A review of calculations of unsteady burning of solid propellants . AIAA J. , 6 ( 12 ), 2241 .
   Google Scholar
• Fletcher , E. A. , and Bunde , G. W. ( 1965 ). An experimental investigation of gas evolution from a solid rocket propellant during pressure transients . AIAA 2nd Aerospace Sciences Meeting , New York , AIAA Paper No. 65-104 .
   Google Scholar
• Fletcher , E. A. , and Bunde , G. W. ( 1966 ). Gas evolution from a solid rocket propellant during depressurization to produce a quench . AIAA J. , 4 ( 1 ), 181 .
   Google Scholar
• Hermance , C. E. ( 1967 ). Continuous measurement of the burning rate of a composite solid propellant . AIAA J. , 5 ( 10 ), 1774 .
   Google Scholar
• Kishore , K. ( 1979 ). Comprehensive view of the combustion models of composite solid propellants . AIAA J. , 17 ( 11 ), 1216 .
   Google Scholar
• Kling , R. , and Brulard , J. ( 1966 ). The regression rates in transient regimes of composite solid propellant grains . La Recherche Aerospatiale , ( 115 ), pp. 1137 – 1144 .
   Google Scholar
• et al. ( 1968 ). Non-steady burning phenomenon of solid propellants . AIAA J. , 6 ( 2 ), 278 .
   Google Scholar
• Krier , H. ( 1969 ). Solid propellant burning in unsteady pressure fields . Ph.D. Thesis , Princeton University .
   Google Scholar
• Kronar , R. N. ( 1973 ). Condensed phase details in the time independent combustion of AP composite propellants . Combustion Science And Technology , 8 , 138 .
   Google Scholar
• Kumar , R. N. ( 1978 ). Lecture Notes from short term course on solid propellant combustion . ISRO-IISc. Joint Program, India; Also AIAA Paper No. 76-699 .
   Google Scholar
• Kuo , Kenneth K. , and Coates , Glen R. ( 1976 ). Review of dynamic burning of solid propellants in gun and rocket propulsion systems . 16th International Symposium on Combustion , pp. 1177 – 1192 .
   Google Scholar
• et al. ( 1972 ). Determination of solid propellant transient regression rates using a microwave Doppler Shift Technique . JPL Technical Report 32-1569 .
   Google Scholar
• et al. ( 1974 ). Microwave Dopper shift technique for determining solid propellant transient regression rates . J. Space Craft and Rockets , 11 ( 2 ), 75 .
   Google Scholar
• Strand , Leon D. , and McNamara ( 1976 ). Development of a variable frequency driver microwave transient regression rate measurement system . AIAA 14th Aerospace Science Meeting, Paper No. 76-105 , Washington , D. C. Also, in Experimental Diagnostics in Gas Solid Phase Combustion Systems , Editor Benn T. Zinn from AIAA Progress in Astronautics and Aeronautics Series .
   Google Scholar
• Strand , Leon D. ( 1979 ). Personal communication .
   Google Scholar
• Cohen , Norman S. ( 1980 ). Review of composite propellant burn rate modelling . AIAA J . 18 ( 3 ), 277 .
   Google Scholar
• Norton , D. J. , and Schultz , A. G. ( 1970 ). Microwave measurement of solid propellants burning rate . JPL Space Programme Summary, 37-65 , 3 , pp. 163 – 167 .
   Google Scholar
• Roache , P. J. ( 1972 ). Computational Fluid Dynamics , Aermosa Publishers , Albuquerque , NM .
   Google Scholar
• Steinz , J. A. , and Selzer , H. ( 1971 ). Depressurization extinguishment of composite solid propellants Flame structure, surface characteristics and restart capability . Combustion Science And Technology , 3 , 25 .
   Web of Science ®Google Scholar
• Summerfeld , M. , and Krier , H. ( 1969 ). Errors in non-steady combustion theory in the past decade (A Review) . AIAA 7th Aerospace Sciences Meeting , New York , AIAA Paper No. 69-178 .
   Google Scholar
• et al. ( 1971 ). Theory of dynamic extinguishment of solid propellant with special reference to nonsteady heat feed back law . J. Spacecraft and Rockets , 8 ( 3 ), 251 .
   Google Scholar
• Suhas , H. K. ( 1981 ). Unsteady combustion of composite propellants subjected to depressurization . Ph.D. Thesis , Indian Institute of Technology , Madras .
   Google Scholar
• Suhas , H. K. , and Bose , T. K. ( 1977 ). A mathematical model to predict transient burning rate and pressure decay rates for extinction of composite propellants . Combustion and Flame , 28 , 145 .
   Google Scholar
• et al. ( 1967 ). Investigation of solid propellant decomposition characteristics and their relation to observed burning rates . AIAA 2nd Solid Propulsion Conference , pp. 136 – 147 .
   Google Scholar
• et al. ( 1969 ). A theoretical and experimental study of propellant combustion phenomenon during rapid depressurization . NASA CR-66733 .
   Google Scholar
• Yin , C. F. , and Hermance , C. E. ( 1971 ). Continuous measurement of transient burning rate of composite propellant undergoing rapid depressurization. AIAA 9th Aerospace Science Meeting , AIAA Paper No. 71-173 .
   Google Scholar