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Influence of element strength and stability on the behavior of SPRE igniter in critical situations

  • Structural Mechanics and Strength of Flight Vehicles
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Abstract

The behavior of the SPRE igniter in critical situations, in which strength and stability properties are exhibited and when performance criteria are changed, is investigated. The possibility to control these situations is proved.

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References

  1. Kalinin, V.V., Kovalev, Yu.N., and Lipanov, A.M., Nestatsionarnye protsessy i metody proektirovaniya uzlov RDTT (Nonstationary Processes and Methods for Design of SPRE Units), Moscow: Mashinostroenie, 1986.

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  2. Repko, V.N., Urazbakhtin, F.A., Yakimovich, B.A., and Orlova, N.Yu., Proektirovanie tekhnicheskikh sistem na osnove analiza uproyadochennykh vo vremeni kriticheskikh sostoyanii (Design of Technical Systems on the Basis of Analyzing Tmie-Ordered Critical Situations), Izhevsk: IzhGTU, 1999.

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  3. Urazbakhtin, F.A. and Korenev, A.A., System of Critical Situation Indicators for Solid Propellant Rocket Engine Igniter, 18-ya Vserossiiskaya mezhdunarodnaya tekhnicheskaya konferentsia: ”Elektromekhanicheskie i vnutrikamernye protsessy v energeticheskikh ustanovkakh, struinaya akustika i diagnostika, pribory i metody kontrolya prirodnoi sredy, veshchestv, materialov i izdelii” (Proc. 18th Int. Tech. Conf.” Electromechanical and Interchamber Processes in Power Plants, Jet Acoustics and Diagnostics, Devices and Methods for Control of Environment, Substances, Materials and Articles”), Kazan: Kazan.Vyssh. Artiler. Komand. Uchilishche, 2006, pp. 324–326.

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Authors and Affiliations

  1. Votkinskii Campus of Izhevsk State Technical University, Votkinsk, Russia

    A. A. Korenev & F. A. Urazbakhtin

Authors
  1. A. A. Korenev
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  2. F. A. Urazbakhtin
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Additional information

Original Russian Text © A.A. Korenev, F.A. Urazbakhtin, 2008, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2008, No. 1, pp. 9–12.

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Korenev, A.A., Urazbakhtin, F.A. Influence of element strength and stability on the behavior of SPRE igniter in critical situations. Russ. Aeronaut. 51, 5–10 (2008). https://doi.org/10.3103/S1068799808010029

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  • DOI: https://doi.org/10.3103/S1068799808010029

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