Detonation burning concepcia application in aviation power-plants


The advantages of a detonation application in aviation power-plant were proved with the thermodynamics point of view. The review of detonation utilization in aviation engine were performed, also the advanced conceptions were selected. Quick information about state of pulse detonation engine research was reported. The issues of pulse detonation engine development were structured and schematically show.

About the authors

1 1

Samara State Aerospace University

Author for correspondence.
Russian Federation


  1. Марчуков Е. Ю., Нечаев Ю. Н., Полев А. С., Тарасов А. И. Второе рождение авиационных пульсирующих двигателей // Полет. 2003. - №4. – С. 43-50.
  2. Нечаев Ю. Н., Тарасов А. И. Новый подход к организации рабочего процесса пульсирующих детонационных двигателей // Полет. 2000. - №8. – С. 3-9.
  3. Работы по пульсирующему детонационному двигателю, проводимые фирмами Дженерал-Электрик, Пратт-Уитни и РоллсРойс // Э.И. Авиационное двигателестроение / ЦИАМ. – 2004. - № 29. – С. 3-6.
  4. Продолжение работ по программе создания детонационного двигателя в США // Аэронавтика и космос. 2006. - №14. – С. 60-61.
  5. Bussing T. R., Hinkey J. B., Kaye, L. “Pulse Detonation Engine Preliminary Design Considerations”. AIAA 94-3200, 30th AIAA/ ASME/SAE/ASEE Joint PropulsionConference, June 1994.
  6. Frankey В., Schauer F., BradleyR.,Hoke J. “Evaluation of a hybrid-piston pulsed detonation engine”. AIAA 2002-0474, 40th AIAA Aerospace Sciences Meeting & Exhibit, 14-17 January 2002.
  7. Ma, F., Choi, J-Y, Wu, Y., Yang, V. In: Roy G, Frolov, S., Santoro, R., Tsyganov, S., editors. Advances in confined detonations. Moscow: Torus Press; 2002. p. 231–4.



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