A model for the combustion and extinction of composite solid propellants during depressurization
In this paper are described some results of an investigation of the transient burning rate and critical pressure decay rate required to cause extinction of a steadily burning solid propellant subject to sudden depressurization. The analysis takes into account the finite times associated with the con...
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| Published in | Combustion and flame Vol. 22; no. 1; pp. 59 - 69 |
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| Main Authors | , |
| Format | Journal Article |
| Language | English |
| Published |
Elsevier Inc
01.01.1974
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| Abstract | In this paper are described some results of an investigation of the transient burning rate and critical pressure decay rate required to cause extinction of a steadily burning solid propellant subject to sudden depressurization. The analysis takes into account the finite times associated with the conduction process and the variation of condensed phase heat release in the solid during a transient. It is postulated that composition of the solid decomposition products,is oxidizer-rich immediately after the start of depressurization and fuel-rich afterwards. The theoretically calculated transient burning rates qualitatively agree with experimentally measured values, reported by Norton and Schultz [1]. Yin and Hermance [2], and Fletcher and Bunde [3]. A stability analysis under the linear approximation predicts the existence of a minimum burning, surface temperature below which stable combustion of the solid propellant is not possible. The analysis correctly predicts the critical depressurization rate required to extinguish a burning solid propellant by sudden preventing of the combustion chamber. |
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| AbstractList | In this paper are described some results of an investigation of the transient burning rate and critical pressure decay rate required to cause extinction of a steadily burning solid propellant subject to sudden depressurization. The analysis takes into account the finite times associated with the conduction process and the variation of condensed phase heat release in the solid during a transient. It is postulated that composition of the solid decomposition products,is oxidizer-rich immediately after the start of depressurization and fuel-rich afterwards. The theoretically calculated transient burning rates qualitatively agree with experimentally measured values, reported by Norton and Schultz [1]. Yin and Hermance [2], and Fletcher and Bunde [3]. A stability analysis under the linear approximation predicts the existence of a minimum burning, surface temperature below which stable combustion of the solid propellant is not possible. The analysis correctly predicts the critical depressurization rate required to extinguish a burning solid propellant by sudden preventing of the combustion chamber. Results of an investigation of the transient burning rate and critical pressure decay rate required to cause extinction of a steadily burning solid propellant subject to sudden depressurization. The analysis takes into account the finite times associated with the conduction process and the variation of condensed phase heat release in the solid during a transient. It is postulated that composition of the solid decomposition products is oxidizer-rich immediately after the start of depressurization and fuel-rich afterwards. The theoretically calculated transient burning rates qualitatively agree with experimentally measured values, reported by Norton and Schultz (1970), Yin and Hermance (1971), and Fletcher and Bunde (1965). A stability analysis under the linear approximation predicts the existence of a minimum burning surface temperature below which stable combustion of the solid propellant is not possible. The analysis correctly predicts the critical depressurization rate required to extinguish a burning solid propellant by sudden venting of the combustion chamber. |
| Author | Mongia, Hukam C. Ambs, Lawrence L. |
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| CitedBy_id | crossref_primary_10_1016_0010_2180_77_90020_7 crossref_primary_10_1016_j_combustflame_2017_05_030 crossref_primary_10_1016_j_dt_2023_07_019 crossref_primary_10_1016_0094_5765_84_90029_8 crossref_primary_10_6108_KSPE_2017_21_5_037 crossref_primary_10_1016_0010_2180_74_90123_0 crossref_primary_10_1002_1097_0363_20000715_33_5_627__AID_FLD931_3_0_CO_2_A |
| Cites_doi | 10.2514/3.4492 10.2514/3.6288 10.2514/8.5727 10.2514/3.4490 10.2514/8.5806 10.1007/BF00741605 10.2514/3.3118 10.21236/AD0697661 |
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| References | Coates (bib19) 1965; 3 Clepluch (bib6) 1964 Mongia Hukam (bib14) 1971 Powling, Smith (bib16) 1965 Andersen, Chaiken (bib18) 1961; 31 Cheng, Baer, Ryan (bib17) 1970 Baer, Schultz, Ryan (bib15) 1971; 9 Zeldovich (bib12) 1963 Pullet, Coffer (bib23) January 20–22, 1969 Clepluch (bib5) 1962; 1559 Merkla, Turk, Summerfield (bib9) 1969 Horton, Bruno, Graesser (bib21) 1968; 6 Summerfield, Caveny, Buttista, Kubota, Gostinatov, Inoda (bib10) June 15–19, 1970 Jensen (bib8) 1969 Novoshilov (bib13) 1967; 3 Yin, Hermance (bib2) 1971 Jenna (bib7) 1967 Clepluch (bib4) 1961; 31 Wooldridge, Marxman (bib11) June 15–19, 1970 Denison, Bauan (bib20) 1961; 31 Norton, Schultz (bib1) 1970; Vol. III Crack, Nicolson (bib24) 1947; 43 Fletcher, Bunde (bib3) 1965 Krier, Tien, Sirignamo, Summerfield (bib22) 1968; 6 Coates (10.1016/0010-2180(74)90010-8_bib19) 1965; 3 Merkla (10.1016/0010-2180(74)90010-8_bib9) 1969 Mongia Hukam (10.1016/0010-2180(74)90010-8_bib14) 1971 Cheng (10.1016/0010-2180(74)90010-8_bib17) 1970 Clepluch (10.1016/0010-2180(74)90010-8_bib4) 1961; 31 Wooldridge (10.1016/0010-2180(74)90010-8_bib11) 1970 Jenna (10.1016/0010-2180(74)90010-8_bib7) 1967 Andersen (10.1016/0010-2180(74)90010-8_bib18) 1961; 31 Jensen (10.1016/0010-2180(74)90010-8_bib8) 1969 Horton (10.1016/0010-2180(74)90010-8_bib21) 1968; 6 Summerfield (10.1016/0010-2180(74)90010-8_bib10) 1970 Novoshilov (10.1016/0010-2180(74)90010-8_bib13) 1967; 3 Krier (10.1016/0010-2180(74)90010-8_bib22) 1968; 6 Crack (10.1016/0010-2180(74)90010-8_bib24) 1947; 43 Fletcher (10.1016/0010-2180(74)90010-8_bib3) 1965 Powling (10.1016/0010-2180(74)90010-8_bib16) 1965 Norton (10.1016/0010-2180(74)90010-8_bib1) 1970; Vol. III Baer (10.1016/0010-2180(74)90010-8_bib15) 1971; 9 Clepluch (10.1016/0010-2180(74)90010-8_bib5) 1962; 1559 Denison (10.1016/0010-2180(74)90010-8_bib20) 1961; 31 Zeldovich (10.1016/0010-2180(74)90010-8_bib12) 1963 Clepluch (10.1016/0010-2180(74)90010-8_bib6) 1964 Yin (10.1016/0010-2180(74)90010-8_bib2) 1971 Pullet (10.1016/0010-2180(74)90010-8_bib23) 1969 |
| References_xml | – volume: 1559 year: 1962 ident: bib5 article-title: Effect of composition on combustion of solid propellants during a rapid pressure decrease publication-title: Nasa Tech. Note D – year: 1967 ident: bib7 article-title: A start-stop study of solid propellants publication-title: NASA CR-66488 – year: 1971 ident: bib14 article-title: A theoretical study of the combustion and extinction of composite solid propellants during depressurization publication-title: Ph.D. dissertation – start-page: 2167 year: 1964 ident: bib6 article-title: Spontaneous registration of previously extinguished solid propellants publication-title: Nasa Tech. 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PMTF – start-page: 2167 year: 1964 ident: 10.1016/0010-2180(74)90010-8_bib6 article-title: Spontaneous registration of previously extinguished solid propellants publication-title: Nasa Tech. Note D – volume: 3 start-page: 19 year: 1967 ident: 10.1016/0010-2180(74)90010-8_bib13 article-title: Stability of the stationary regime in a semi-confined space publication-title: Combustion, Explosion Shock Waves doi: 10.1007/BF00741605 – volume: 3 start-page: 125 year: 1965 ident: 10.1016/0010-2180(74)90010-8_bib19 article-title: Linear pyrolysis rate measurements of propellant constituents publication-title: AIAA J. doi: 10.2514/3.3118 – start-page: 1373 year: 1965 ident: 10.1016/0010-2180(74)90010-8_bib16 article-title: The surface temperature of ammonium perchlorate burning at elevated pressures – year: 1969 ident: 10.1016/0010-2180(74)90010-8_bib9 article-title: Extinguishment of solid propellants by rapid depressurization doi: 10.21236/AD0697661 |
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