Theoretical Analysis of the Composition and Thermodynamic Parameters of Products Formed in Combustion of 2,2'-Bis(bicyclo[2.2.1]heptane) in Oxygen
Theoretical analysis was made on the composition and thermodynamic parameters of combustion products of 2,2'-bis(bicyclo[2.2.1]heptane) in oxygen in a wide range of temperatures and pressures. 2,2'-Bis(bicyclo[2.2.1]heptane) can potentially be used as a fuel component in combustion chamber...
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| Veröffentlicht in: | Russian journal of applied chemistry 2019-09, Vol.92 (9), p.1284-1290 |
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| container_end_page | 1290 |
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| container_title | Russian journal of applied chemistry |
| container_volume | 92 |
| creator | Bermeshev, M. V. Kochetov, I. V. Pevgov, V. G. Samoilov, V. O. Shorunov, S. V. |
| description | Theoretical analysis was made on the composition and thermodynamic parameters of combustion products of 2,2'-bis(bicyclo[2.2.1]heptane) in oxygen in a wide range of temperatures and pressures. 2,2'-Bis(bicyclo[2.2.1]heptane) can potentially be used as a fuel component in combustion chambers of liquid rocket engines for the first-stage launch vehicles. The average molar mass of approximately 26 amu., obtained for products formed in combustion of 2,2'-bis(bicyclo[2.2.1]heptane) in oxygen is close to similar values for methane in oxygen, whereas its density is more than twice the density of liquid methane. This circumstance makes it possible to hope that the mass of storage tanks can be made smaller if 2,2'-bis(bicyclo[2.2.1]heptane) is used for rockets, compared with the mass of storage tanks containing an equivalent amount of methane. The results obtained can be used to calculate nozzle profiles and combustion chamber parameters of a liquid jet propulsion engines. |
| doi_str_mv | 10.1134/S1070427219090143 |
| format | Article |
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V. ; Kochetov, I. V. ; Pevgov, V. G. ; Samoilov, V. O. ; Shorunov, S. V.</creator><creatorcontrib>Bermeshev, M. V. ; Kochetov, I. V. ; Pevgov, V. G. ; Samoilov, V. O. ; Shorunov, S. V.</creatorcontrib><description>Theoretical analysis was made on the composition and thermodynamic parameters of combustion products of 2,2'-bis(bicyclo[2.2.1]heptane) in oxygen in a wide range of temperatures and pressures. 2,2'-Bis(bicyclo[2.2.1]heptane) can potentially be used as a fuel component in combustion chambers of liquid rocket engines for the first-stage launch vehicles. The average molar mass of approximately 26 amu., obtained for products formed in combustion of 2,2'-bis(bicyclo[2.2.1]heptane) in oxygen is close to similar values for methane in oxygen, whereas its density is more than twice the density of liquid methane. This circumstance makes it possible to hope that the mass of storage tanks can be made smaller if 2,2'-bis(bicyclo[2.2.1]heptane) is used for rockets, compared with the mass of storage tanks containing an equivalent amount of methane. The results obtained can be used to calculate nozzle profiles and combustion chamber parameters of a liquid jet propulsion engines.</description><identifier>ISSN: 1070-4272</identifier><identifier>EISSN: 1608-3296</identifier><identifier>DOI: 10.1134/S1070427219090143</identifier><language>eng</language><publisher>Moscow: Pleiades Publishing</publisher><subject>Aerospace engines ; Chemistry ; Chemistry and Materials Science ; Chemistry/Food Science ; Combustion chambers ; Combustion products ; Composition ; Density ; Heptanes ; Industrial Chemistry/Chemical Engineering ; Jet propulsion ; Methane ; Nozzles ; Oxygen ; Parameters ; Physicochemical Studies of Systems and Processes ; Rocket engines ; Rockets ; Storage tanks</subject><ispartof>Russian journal of applied chemistry, 2019-09, Vol.92 (9), p.1284-1290</ispartof><rights>Pleiades Publishing, Ltd. 2019</rights><rights>Copyright Springer Nature B.V. 2019</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><cites>FETCH-LOGICAL-c305t-2c375d915272f8730e58c4c44ca60d90593675755632c393d3166e9043b403d53</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://link.springer.com/content/pdf/10.1134/S1070427219090143$$EPDF$$P50$$Gspringer$$H</linktopdf><linktohtml>$$Uhttps://link.springer.com/10.1134/S1070427219090143$$EHTML$$P50$$Gspringer$$H</linktohtml><link.rule.ids>314,776,780,27901,27902,41464,42533,51294</link.rule.ids></links><search><creatorcontrib>Bermeshev, M. 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The average molar mass of approximately 26 amu., obtained for products formed in combustion of 2,2'-bis(bicyclo[2.2.1]heptane) in oxygen is close to similar values for methane in oxygen, whereas its density is more than twice the density of liquid methane. This circumstance makes it possible to hope that the mass of storage tanks can be made smaller if 2,2'-bis(bicyclo[2.2.1]heptane) is used for rockets, compared with the mass of storage tanks containing an equivalent amount of methane. The results obtained can be used to calculate nozzle profiles and combustion chamber parameters of a liquid jet propulsion engines.</description><subject>Aerospace engines</subject><subject>Chemistry</subject><subject>Chemistry and Materials Science</subject><subject>Chemistry/Food Science</subject><subject>Combustion chambers</subject><subject>Combustion products</subject><subject>Composition</subject><subject>Density</subject><subject>Heptanes</subject><subject>Industrial Chemistry/Chemical Engineering</subject><subject>Jet propulsion</subject><subject>Methane</subject><subject>Nozzles</subject><subject>Oxygen</subject><subject>Parameters</subject><subject>Physicochemical Studies of Systems and Processes</subject><subject>Rocket engines</subject><subject>Rockets</subject><subject>Storage tanks</subject><issn>1070-4272</issn><issn>1608-3296</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2019</creationdate><recordtype>article</recordtype><recordid>eNp1kM1KAzEURgdRsFYfwF3AhQpOvfmdybIWq4LQgnUlMqSZtE3pTGoyBec1fGLTVnAhru6Fe84H90uScww9jCm7fcGQASMZwRIkYEYPkg4WkKeUSHEY93hOt_fj5CSEJQBIIfJO8jVZGOdNY7VaoX6tVm2wAbkZahYGDVy1dsE21tVI1SWKrK9c2daqshqNlVeVaYzf8WPvyo1uAho6X5kS2XqrTzdhZ0eA3JDL9M6Gq6nVrV65N9IjPfy-MOtG1eZ6K4w-27mpT5OjmVoFc_Yzu8nr8H4yeEyfRw9Pg_5zqinwJiWaZryUmMenZnlGwfBcM82YVgJKCVxSkfGMc0EjKmlJsRBGAqNTBrTktJtc7HPX3n1sTGiKpdv4WEEoCIVcMCEljhTeU9q7ELyZFWtvK-XbAkOxrb74U310yN4Jka3nxv8m_y99Azvzg9o</recordid><startdate>20190901</startdate><enddate>20190901</enddate><creator>Bermeshev, M. 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The average molar mass of approximately 26 amu., obtained for products formed in combustion of 2,2'-bis(bicyclo[2.2.1]heptane) in oxygen is close to similar values for methane in oxygen, whereas its density is more than twice the density of liquid methane. This circumstance makes it possible to hope that the mass of storage tanks can be made smaller if 2,2'-bis(bicyclo[2.2.1]heptane) is used for rockets, compared with the mass of storage tanks containing an equivalent amount of methane. The results obtained can be used to calculate nozzle profiles and combustion chamber parameters of a liquid jet propulsion engines.</abstract><cop>Moscow</cop><pub>Pleiades Publishing</pub><doi>10.1134/S1070427219090143</doi><tpages>7</tpages></addata></record> |
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| subjects | Aerospace engines Chemistry Chemistry and Materials Science Chemistry/Food Science Combustion chambers Combustion products Composition Density Heptanes Industrial Chemistry/Chemical Engineering Jet propulsion Methane Nozzles Oxygen Parameters Physicochemical Studies of Systems and Processes Rocket engines Rockets Storage tanks |
| title | Theoretical Analysis of the Composition and Thermodynamic Parameters of Products Formed in Combustion of 2,2'-Bis(bicyclo[2.2.1]heptane) in Oxygen |
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