DESIGN, MANUFACTURING, COLD AND HOT-FIRE TEST OF A LIQUID SUBSCALE ENGINE WITH SINGLE SWIRL DOUBLE BASE INJECTOR

Q: How can I download an article?

To download an article from SID, first log in to the site, search for the article title, and click on the 'Download Article' option.

Q: How can I download an ISI article?

To download an ISI article on SID, enter the keyword or article title in the search bar, view the relevant results, click on the desired article, and select the 'Download Article' option.

Q: How can I access the SID database?

To access the SID database, visit SID.ir, create an account, and log in to access scientific resources.

Q: Is downloading articles from SID free?

Some articles on SID are available for free, while others require payment. Details are specified on the article's page.

MEHRABI A.; OMMI F.; VALIZADEH S.; MOVAHEDNEJAD E.

Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Journal Paper

Paper Information

Journal: JOURNAL OF MECHANICAL ENGINEERING AMIRKABIR (AMIRKABIR) Year:2016 | Volume:48 | Issue:1 Page(s): 25-28

Download Full-Text

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Persian Verion

View:

872

Download:

729

Cites:

Information Journal Paper

Title

DESIGN, MANUFACTURING, COLD AND HOT-FIRE TEST OF A LIQUID SUBSCALE ENGINE WITH SINGLE SWIRL DOUBLE BASE INJECTOR

Author(s)

MEHRABI A. | OMMI F. | VALIZADEH S. | MOVAHEDNEJAD E. | Issue Writer Certificate

Keywords

DOUBLE BASE SWIRL INJECTORQ2

SUBSCALE ENGINEQ2

LIQUID PROPELLANTQ2

COLD & HOT-FIRE TESTQ2

Abstract

The ongoing developmental studies on the application of subscale liquid rocket engines as small thruster and laboratory tester are briefly reviewed. Then a detailed design and manufacturing process of a laboratory liquid SUBSCALE ENGINE with single swirl double base injector of 300 N thrust for this reaserch is presented. For the preparation of pressurized water, fuel and oxide, a test facility has been prepared. Results of water analogy tests are presented. Initial firings using the real fuel and oxide were not successful. Low fuel flow, low mixing area of the fuel and oxide, and contamination in the TR-1 were considered to be the reasons. Overcoming to these problems resulted in successful firing of the SUBSCALE ENGINE. Obtained results were adapted to design expected results.

Cites

No record.

References

No record.

Cite

APA: Copy

MEHRABI, A., OMMI, F., VALIZADEH, S., & MOVAHEDNEJAD, E.. (2016). DESIGN, MANUFACTURING, COLD AND HOT-FIRE TEST OF A LIQUID SUBSCALE ENGINE WITH SINGLE SWIRL DOUBLE BASE INJECTOR. JOURNAL OF MECHANICAL ENGINEERING AMIRKABIR (AMIRKABIR), 48(1), 25-28. SID. https://sid.ir/paper/358904/en

Vancouver: Copy

MEHRABI A., OMMI F., VALIZADEH S., MOVAHEDNEJAD E.. DESIGN, MANUFACTURING, COLD AND HOT-FIRE TEST OF A LIQUID SUBSCALE ENGINE WITH SINGLE SWIRL DOUBLE BASE INJECTOR. JOURNAL OF MECHANICAL ENGINEERING AMIRKABIR (AMIRKABIR)[Internet]. 2016;48(1):25-28. Available from: https://sid.ir/paper/358904/en

IEEE: Copy

A. MEHRABI, F. OMMI, S. VALIZADEH, and E. MOVAHEDNEJAD, “DESIGN, MANUFACTURING, COLD AND HOT-FIRE TEST OF A LIQUID SUBSCALE ENGINE WITH SINGLE SWIRL DOUBLE BASE INJECTOR,” JOURNAL OF MECHANICAL ENGINEERING AMIRKABIR (AMIRKABIR), vol. 48, no. 1, pp. 25–28, 2016, [Online]. Available: https://sid.ir/paper/358904/en

Related Journal Papers