2012
DOI: 10.6108/kspe.2012.16.1.009 View full text |Buy / Rent full text
|
|

Abstract: An unsteady internal ballistic performance model was proposed to take account for the variance of local regression rate along the grain port of a hybrid rocket combustor. The characteristic parameters of hybrid rocket motor was investigated. The performance model of concern in the study was fairly comparable with the test result. The combustion coefficients and local burning characteristics of a hybrid rocket motor were evaluated. The local variation of the oxidizer mass flow rate results in the changes of loc… Show more

Help me understand this report

Search citation statements

Order By: Relevance
Select...
0
0
0

Publication Types

Select...

Relationship

0
0

Authors

Journals