ARTICLE
Investigation of an additional oxidizer charge effect on selected operational characteristics of a solid-fuel rocket engine
 
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Air Force Institute of Technology, Warsaw, Poland
 
Journal of Theoretical and Applied Mechanics 2014;52(1):139–149
 
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ABSTRACT
The paper has been intended to discuss some issues closely related to the elimination of an extremely disadvantageous phenomenon, i.e. the occurrence of a negative oxygen balance in products of combustion emitted by a solid-fuel rocket engine while launching a missile from the aircraft. Findings of experimental examination of such engines furnished with an additional oxidizer charge have also been presented.
eISSN:2543-6309
ISSN:1429-2955