Abstract
The possibility of replacing the currently widely used ammonium perchlorate as an oxidizing agent (dispersant) in the composition of solid boron-containing fuels for aircraft with rocket ramjet engine was considered by dispersants with reduced nitrogen and oxygen content with a high enthalpy of formation (more than 2 MJ kg−1) and capable of gasifying solid fuels. The efficiency of fuels with high enthalpy dispersants was evaluated in an optimization setting according to the flight range criterion of the aircraft taking into account the complete combustion of fuel in the afterburner chamber. A number of the most effective dispersants were recommended for further study.
This is a preview of subscription content, log in via an institution to check access.
Similar content being viewed by others
References
Aleksandrov, V.N., Bytskevich, V.M., Verkholomov, V.K., Gramenitskiy, M.D., Dulepov, N.P., Skibin, V.A., Surikov, Ye., V., Khil’kevich, V.Ya., and Yanovskiy, L.S., Integral’nye pryamotochnye vozdushno-reaktivnye dvigateli na tverdykh toplivakh (Osnovy teorii rascheta) [Integral Ramjet Engines on Solid Fuels (Fundamentals of the Theory of Calculation)], Moscow: Akademkniga, 2006.
Kalpakli, B., Acar, E.B., and Ulas, A., Combust. Flame, 2017, vol. 179,, pp. 267–279.
Sorokin, V.A., Yanovskiy, L.S., Kozlov, V.A., Surikov, Ye.V., Sharov, M.S., Fel’dman, V.D., Frantskevich, V.P., Zhivotov, N.P., Abashev, V.M., and Chervakov, V.V., Raketno-pryamotochnye dvigateli na tverdykh i pastoobraznykh toplivakh. Osnovy proektirovaniya i eksperimental’noi otrabotki (Rocket and Ramjet Engines on Solid and Pasty Fuels. Fundamentals of Design and Experimental Development), Moscow: Fizmatlit, 2010.
Sorokin, V.A., Yanovskiy, L.S., Yagodnikov, D.A., Frantskevich, V.P., Surikov, Ye.V., Raznoschikov, V.V., Zakharov, N.N., Tikhomirov, M.A., and Sharov, M.S., Proektirovaniye i otrabotka raketno-pryamotochnykh dvigatelei na tverdom toplive: Ucheb. Posobie (Design and Development of Solid-Fuel Rocket Engines: A Textbook), Sorokin, V.A., Ed., Moscow: MGTU im. N. E. Baumana, 2016.
Obnosov, B.V., Sorokin, V.A., Yanovskiy, L.S., Yagodnikov, D.A., Frantskevich, V.P., Zhivotov, N.P., Surikov, Ye.V., Kobko, G.G., Tikhomirov, M.A., and Sharov, M.S., Konstruktsiya i proektirovanie kombinirovannykh raketnykh dvigatelei na tverdom toplive (Design of Combined Solid-Fuel Rocket Engines), Sorokin, V.A., Ed., Moscow: MGTU im. N. E. Baumana, 2012.
Athawale, V.K., Asthana, S.N., and Singh, H., Defence Sci. J., 1994, vol. 44, no. 4, pp. 269–278.
Mitsuno, M., Kuwahara, T., Kosaka, K., and Kubota, N., 23rd Joint Propulsion Conf., 1987.
Chen, B., Xia, Z., Huang, L., and Ma, L., Aerospace Sci. Technol., 2018, vol. 82–83, pp. 210–219.
Lebedev, A.A. and Chernobrovkin, L.S., Dinamika poleta bespilotnykh letatel’nykh apparatov: Ucheb. posobie dlya vuzov (Dynamics of Flight of Unmanned Aerial Vehicles: Textbook for Universities), Moscow: Mashinostroenie, 1973.
Yugov, O.K. and Selivanov, O.D., Osnovy integratsii samoleta i dvigatelya (Basics of Aircraft and Engine Integration), Yugov, O.K., Ed., Moscow: Mashinostroenie, 1989.
Gany, A. and Netzer, D.W., Int. J. TurboJet-Engines, 1985, vol. 2, no. 2, pp. 157–168.
Raznoschikov, V.V., Polet, 2008, no. 4, pp. 28–32.
Dulepov, N.P., Kotenkov, G.K., and Yanovskiy, L.S., Aktual’nye problemy aviatsionnykh i aerokosmicheskikh sistem: protsessy, modeli, eksperiment (Actual Problems of Aviation and Aerospace Systems: Processes, Models, Experiment), 2001, vol. 6, no. 2(12), pp. 1–21.
Dulepov, N.P., Kotenkov, G.K., and Yanovskiy, L.S., Vestn. Ros. Akad. Kosmonavtiki im. K. E. Tsiol, kovskogo, 1999, no. 4, pp. 86–91.
Orlov, B.V., Mazing, G.Yu., Reydel, A.L., Stepanov, M.N., and Topcheyev, Yu.I., Osnovy proektirovaniya raketno-pryamotochnykh dvigatelei dlya bespilotnykh letatel’nykh apparatov (Fundamentals of Rocket Engine Design for Unmanned Aircrafts), Moscow: Mashinostroyeniye, 1967.
Zuyev, V.S. and Makaron, V.S., Teoriya pryamotochnykh i raketno-pryamotochnykh dvigatelei (Theory of Ramjet and Rocket Ramjet Engines), Moscow: Mashino stroenie, 1971.
Kurziner, R.I., Reaktivnye dvigateli dlya bol’shikh sverkh-zvukovykh skorostei poleta (Jet Engines for High Super sonic Flight Speeds), Moscow: Mashino stroyeniye, 1977.
Trusov, B.G., Abstracts of Papers, III Mezhdunar. simp. “Gorenie i plazmokhimiya,” (3rd Int. Symp on Combustion and Plasma Chemistry), Almaty: Kazak Iniv., 2005, pp. 52–57.
Abugov, D.I. and Bobylev, V.M., Teoriya i raschet raketnykh dvigatelei tverdogo topliva (Theory and Calculation of Solid Fuel Rocket Engines), Moscow: Mashinostroyeniye, 1987.
Sosounov, V.A., tResearch and Development of Ram/Scramjets and Turboramjets in Russia: AGARD Lecture Ser. 194, Loughton, 1994, pp. 10–12.
Bathelt, H., Volk, F., and Weidel, M., ICT-Database of Thermo chemical Values. Version 7.0, Fraunhofer Institut fur Chem. Technologie. Pfintztal, 2004.
Acknowledgments
The authors are grateful to V.A. Stepanov (FGUP TsIAM named for P. I. Baranov) for the information on the characteristics of the supersonic intake device.
Author information
Authors and Affiliations
Corresponding author
Rights and permissions
About this article
Cite this article
Yanovskii, L.S., Lempert, D.B., Raznoschikov, V.V. et al. Evaluation of Effectiveness of Solid Fuels Based on High Enthalpy Dispersants for Rocket Ramjet Engines. Russ J Appl Chem 92, 367–388 (2019). https://doi.org/10.1134/S1070427219030078
Received:
Revised:
Accepted:
Published:
Issue Date:
DOI: https://doi.org/10.1134/S1070427219030078