Abstract A method for shaping a supersonic part of a compact multinozzle cluster of a solid propellant rocket engine (SPRE) with out-of-round nozzles integrated into the common bell mouth is proposed. Also presented is an approach to evaluation of basic components of the total thrust impulse losses.
Shaping a SPRE multinozzle cluster with out-of-round nozzles
Russian Aeronautics (Iz VUZ) ; 53 , 2 ; 202-205
2010-06-01
4 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Shaping a SPRE multinozzle cluster with out-of-round nozzles
Online Contents | 2010
|Racheta spre spaţiile planetare
TIBKAT | 2003
|Thermoacoustic Coupling in a Multinozzle Staged Combustor
Online Contents | 2016
|Helical Flow Disturbances in a Multinozzle Combustor
Online Contents | 2015
|