Thebasic problems of application of detonation process in propulsion systemswith impulse and continuous burning of combustible\r\nmixture are discussed.The results on propagation of detonation waves in supersonic flow are analyzed relatively to air-breathing\r\nengine. The experimental results are presented showing the basic possibility of creation of an engine with exterior detonation\r\nburning. The base results on optimization of initiation in impulse detonation engine are explained at the expense of spatial and\r\ntemporal redistribution of an energy, entered into a mixture. The method and technique for construction of highly effective\r\naccelerators for deflagration to detonation transition are discussed also.
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