The energy potential of some high-enthalpy N-oxides as oxidizers
The energy abilities of solid composite propellants based on a couple of new high-enthalpy N-oxides (furazano-terazine-dioxide and tetrazino-tetrazine-1,3,6,8-tetraoxide) have been considered, it is found that these two compounds show record energy characteristics — specific impulse up to 273 s (a...
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Main Authors: | , , |
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Format: | Article |
Language: | English |
Published: |
Omsk State Technical University, Federal State Autonomous Educational Institution of Higher Education
2018-10-01
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Series: | Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение" |
Subjects: | |
Online Access: | https://www.omgtu.ru/general_information/media_omgtu/journal_of_omsk_research_journal/files/arhiv/2018/%D0%A2.%202,%20%E2%84%96%203/58-62%20%D0%9B%D0%B5%D0%BC%D0%BF%D0%B5%D1%80%D1%82%20%D0%94.%20%D0%91.,%20%D0%94%D0%BE%D1%80%D0%BE%D1%84%D0%B5%D0%B5%D0%BD%D0%BA%D0%BE%20%D0%95.%20%D0%9C.,%20%D0%A1%D0%BE%D0%B3%D0%BB%D0%B0%D1%81%D0%BD%D0%BE%D0%B2%D0%B0%20%D0%A1.%20%D0%98..pdf |
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Summary: | The energy abilities of solid composite propellants based on a couple of new high-enthalpy N-oxides
(furazano-terazine-dioxide and tetrazino-tetrazine-1,3,6,8-tetraoxide) have been considered, it is found that
these two compounds show record energy characteristics — specific impulse up to 273 s (at pressure in the
combustion chamber and at the nozzle section 4,0 and 0,1 MPa respectively) at the combustion temperature
not higher than 3700 K. Formulations based on these two compounds are very powerful if any binder
(an active binder or a hydrocarbon one) is used |
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ISSN: | 2588-0373 2587-764X |