
Multicriterial choice of the best variant of the pulse detonation engine design for aircraft angular stabilization and orientation systems
Author(s) -
В. В. Сафронов,
В. А. Поршнев,
А. С. Жебраков
Publication year - 2014
Publication title -
vestnik samarskogo universiteta. aèrokosmičeskaâ tehnika, tehnologii i mašinostroenie
Language(s) - English
Resource type - Journals
eISSN - 2541-7533
pISSN - 2542-0453
DOI - 10.18287/1998-6629-2014-0-5-2(47)-22-34
Subject(s) - detonation , pulse (music) , ranging , thrust specific fuel consumption , orientation (vector space) , mechanics , computer science , fuel efficiency , automotive engineering , mathematics , engineering , physics , chemistry , geometry , explosive material , telecommunications , organic chemistry , detector