Simultaneous Temperature and Species Measurements During Self-Oscillating Burning of HMX
The near-surface species and surface temperature were simultaneously measured during self-oscillatory burning of octahydro-1,3,5,7-tetranitro-1,3,5,7-tetrazocine (HMX). A CO2 laser was used to heat the propellant surface at atmospheric pressure in argon. A microprobe/triple quadrupole mass spectrome...
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Veröffentlicht in: | Journal of propulsion and power 1999-03, Vol.15 (2), p.296-303 |
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description | The near-surface species and surface temperature were simultaneously measured during self-oscillatory burning of octahydro-1,3,5,7-tetranitro-1,3,5,7-tetrazocine (HMX). A CO2 laser was used to heat the propellant surface at atmospheric pressure in argon. A microprobe/triple quadrupole mass spectrometer system was used to measure species profiles, and fine-wire thermocouples were used to measure surface temperature. Oscillations of species, temperature, and burning rate were observed with an average surface temperature of 4633 K and frequency of 4 +/- 0.2 Hz. The mole fraction of NO2, HCN, and triazine oscillated in phase with temperature, whereas the mole fractions of N2O, CH2O, and the species at mass 28 were 180 deg out of phase with temperature. NO2 and CH2O were the most abundant species, followed by HCN, N2O, H2O, the species at mass 28, and other species. The production of NO2 and HCN was favored with an increase in temperature and burning rate, whereas the production of N2O and CH2O became more important with a decrease in temperature and burning rate. This was qualitatively in line with the accepted global reaction branches in the condensed phase of HMX. From these data, variations of the mole fractions of NO2, N2O, CH2O, and HCN could be directly related to surface temperature. Analysis of the data indicates that the observed oscillatory burning might be related to multiple-step reactions in the condensed phase. (Author) |
doi_str_mv | 10.2514/2.5427 |
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A CO2 laser was used to heat the propellant surface at atmospheric pressure in argon. A microprobe/triple quadrupole mass spectrometer system was used to measure species profiles, and fine-wire thermocouples were used to measure surface temperature. Oscillations of species, temperature, and burning rate were observed with an average surface temperature of 4633 K and frequency of 4 +/- 0.2 Hz. The mole fraction of NO2, HCN, and triazine oscillated in phase with temperature, whereas the mole fractions of N2O, CH2O, and the species at mass 28 were 180 deg out of phase with temperature. NO2 and CH2O were the most abundant species, followed by HCN, N2O, H2O, the species at mass 28, and other species. The production of NO2 and HCN was favored with an increase in temperature and burning rate, whereas the production of N2O and CH2O became more important with a decrease in temperature and burning rate. This was qualitatively in line with the accepted global reaction branches in the condensed phase of HMX. From these data, variations of the mole fractions of NO2, N2O, CH2O, and HCN could be directly related to surface temperature. Analysis of the data indicates that the observed oscillatory burning might be related to multiple-step reactions in the condensed phase. (Author)</description><identifier>ISSN: 0748-4658</identifier><identifier>EISSN: 1533-3876</identifier><identifier>DOI: 10.2514/2.5427</identifier><language>eng</language><publisher>Reston: American Institute of Aeronautics and Astronautics</publisher><subject>Combustion ; Condensation ; Cyanides ; HMX ; Mass spectrometry ; Mass transfer ; Nitrogen oxides ; Rocket engines ; Thermal variables measurement ; Thermocouples ; Water</subject><ispartof>Journal of propulsion and power, 1999-03, Vol.15 (2), p.296-303</ispartof><rights>Copyright American Institute of Aeronautics and Astronautics Mar/Apr 1999</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a373t-fe19b798bd959e27337828ea917840a645db2062ce3951f5d4a79bbf0d121d163</citedby><cites>FETCH-LOGICAL-a373t-fe19b798bd959e27337828ea917840a645db2062ce3951f5d4a79bbf0d121d163</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,27924,27925</link.rule.ids></links><search><creatorcontrib>Tang, Ching-Jen</creatorcontrib><creatorcontrib>Lee, YoungJoo</creatorcontrib><creatorcontrib>Litzinger, Thomas A</creatorcontrib><title>Simultaneous Temperature and Species Measurements During Self-Oscillating Burning of HMX</title><title>Journal of propulsion and power</title><description>The near-surface species and surface temperature were simultaneously measured during self-oscillatory burning of octahydro-1,3,5,7-tetranitro-1,3,5,7-tetrazocine (HMX). A CO2 laser was used to heat the propellant surface at atmospheric pressure in argon. A microprobe/triple quadrupole mass spectrometer system was used to measure species profiles, and fine-wire thermocouples were used to measure surface temperature. Oscillations of species, temperature, and burning rate were observed with an average surface temperature of 4633 K and frequency of 4 +/- 0.2 Hz. The mole fraction of NO2, HCN, and triazine oscillated in phase with temperature, whereas the mole fractions of N2O, CH2O, and the species at mass 28 were 180 deg out of phase with temperature. NO2 and CH2O were the most abundant species, followed by HCN, N2O, H2O, the species at mass 28, and other species. The production of NO2 and HCN was favored with an increase in temperature and burning rate, whereas the production of N2O and CH2O became more important with a decrease in temperature and burning rate. This was qualitatively in line with the accepted global reaction branches in the condensed phase of HMX. From these data, variations of the mole fractions of NO2, N2O, CH2O, and HCN could be directly related to surface temperature. Analysis of the data indicates that the observed oscillatory burning might be related to multiple-step reactions in the condensed phase. (Author)</description><subject>Combustion</subject><subject>Condensation</subject><subject>Cyanides</subject><subject>HMX</subject><subject>Mass spectrometry</subject><subject>Mass transfer</subject><subject>Nitrogen oxides</subject><subject>Rocket engines</subject><subject>Thermal variables measurement</subject><subject>Thermocouples</subject><subject>Water</subject><issn>0748-4658</issn><issn>1533-3876</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1999</creationdate><recordtype>article</recordtype><recordid>eNp9kUtLw0AUhQdRsFb9DQFB3aRm3pml1keFli5aobthktyRlLycSUD_vYkVFBVXB879ONzDQegURxPCMbsiE86I3EMjzCkNaSzFPhpFksUhEzw-REfeb6MIi1jIEdqs8rIrWlNB3flgDWUDzrSdg8BUWbBqIM3BBwswvvdKqFof3HYur56DFRQ2XPo0LwrTDsZN56pBaxvMFptjdGBN4eHkU8fo6f5uPZ2F8-XD4_R6HhoqaRtawCqRKk4yxRUQSamMSQxGYRmzyAjGs4REgqRAFceWZ8xIlSQ2yjDBGRZ0jC52uY2rXzrwrS5zn0L_1EclLZmgGBMpe_L8X5JITBRnA3j2A9zWfbe-hSa0Z0RPfotLXe29A6sbl5fGvWkc6WEITfQwxFecyY35ivpFXf5F7a66yay2XVG08NrSd8Dwkk0</recordid><startdate>19990301</startdate><enddate>19990301</enddate><creator>Tang, Ching-Jen</creator><creator>Lee, YoungJoo</creator><creator>Litzinger, Thomas A</creator><general>American Institute of Aeronautics and Astronautics</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope><scope>7TC</scope></search><sort><creationdate>19990301</creationdate><title>Simultaneous Temperature and Species Measurements During Self-Oscillating Burning of HMX</title><author>Tang, Ching-Jen ; Lee, YoungJoo ; Litzinger, Thomas A</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a373t-fe19b798bd959e27337828ea917840a645db2062ce3951f5d4a79bbf0d121d163</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1999</creationdate><topic>Combustion</topic><topic>Condensation</topic><topic>Cyanides</topic><topic>HMX</topic><topic>Mass spectrometry</topic><topic>Mass transfer</topic><topic>Nitrogen oxides</topic><topic>Rocket engines</topic><topic>Thermal variables measurement</topic><topic>Thermocouples</topic><topic>Water</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Tang, Ching-Jen</creatorcontrib><creatorcontrib>Lee, YoungJoo</creatorcontrib><creatorcontrib>Litzinger, Thomas A</creatorcontrib><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Mechanical Engineering Abstracts</collection><jtitle>Journal of propulsion and power</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Tang, Ching-Jen</au><au>Lee, YoungJoo</au><au>Litzinger, Thomas A</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Simultaneous Temperature and Species Measurements During Self-Oscillating Burning of HMX</atitle><jtitle>Journal of propulsion and power</jtitle><date>1999-03-01</date><risdate>1999</risdate><volume>15</volume><issue>2</issue><spage>296</spage><epage>303</epage><pages>296-303</pages><issn>0748-4658</issn><eissn>1533-3876</eissn><abstract>The near-surface species and surface temperature were simultaneously measured during self-oscillatory burning of octahydro-1,3,5,7-tetranitro-1,3,5,7-tetrazocine (HMX). A CO2 laser was used to heat the propellant surface at atmospheric pressure in argon. A microprobe/triple quadrupole mass spectrometer system was used to measure species profiles, and fine-wire thermocouples were used to measure surface temperature. Oscillations of species, temperature, and burning rate were observed with an average surface temperature of 4633 K and frequency of 4 +/- 0.2 Hz. The mole fraction of NO2, HCN, and triazine oscillated in phase with temperature, whereas the mole fractions of N2O, CH2O, and the species at mass 28 were 180 deg out of phase with temperature. NO2 and CH2O were the most abundant species, followed by HCN, N2O, H2O, the species at mass 28, and other species. The production of NO2 and HCN was favored with an increase in temperature and burning rate, whereas the production of N2O and CH2O became more important with a decrease in temperature and burning rate. This was qualitatively in line with the accepted global reaction branches in the condensed phase of HMX. From these data, variations of the mole fractions of NO2, N2O, CH2O, and HCN could be directly related to surface temperature. Analysis of the data indicates that the observed oscillatory burning might be related to multiple-step reactions in the condensed phase. (Author)</abstract><cop>Reston</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/2.5427</doi><tpages>8</tpages></addata></record> |
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source | Alma/SFX Local Collection |
subjects | Combustion Condensation Cyanides HMX Mass spectrometry Mass transfer Nitrogen oxides Rocket engines Thermal variables measurement Thermocouples Water |
title | Simultaneous Temperature and Species Measurements During Self-Oscillating Burning of HMX |
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