2017
DOI: 10.6108/kspe.2017.21.4.001
|View full text |Cite
|
Sign up to set email alerts
|

One Dimensional Analysis on Alcohol Burner Flow for Turbopump Operation

Abstract: TPTF (Turbopump Real Propellant Test Facility) at Naro Space Center has used alcohol burner system to simulate the gas flow of gas generator of liquid rocket engine. During the test at TPTF, the temperature and pressure at turbine inlet were smoothly increased while those of the gas generator of engine were constant. Present research developed a simulation code for the burner and the piping system and applied to the system. The calculation results were in good agreement with the test, and confirmed quantitativ… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...

Citation Types

0
0
0

Publication Types

Select...

Relationship

0
0

Authors

Journals

citations
Cited by 0 publications
references
References 2 publications
0
0
0
Order By: Relevance

No citations

Set email alert for when this publication receives citations?