EXPERIMENTAL INVESTIGATION OF BURNING RATE OF RDX/AP/AL/HTPB NITRAMINE PROPELLANTS

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.

KARIMI N.; VAZIRI S.A.; DEHNAVI M.A.

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

Journal Paper

Paper Information

Journal: JOURNAL OF ENERGETIC MATERIALS Year:2015 | Volume:9 | Issue:3 (24) Page(s): 49-56

Download Full-Text

Persian Verion

View:

885

Download:

Cites:

Information Journal Paper

Title

EXPERIMENTAL INVESTIGATION OF BURNING RATE OF RDX/AP/AL/HTPB NITRAMINE PROPELLANTS

Author(s)

KARIMI N. | VAZIRI S.A. | DEHNAVI M.A. | Issue Writer Certificate

Keywords

NITRAMINE PROPELLANTSQ2

BURNING RATEQ3

CALORIMETRIC VALUEQ2

APQ2

RDXQ3

Abstract

In this study, the combustion characteristics and BURNING RATE of RDX/AP/Al/HTPB composite solid propellant were studied experimentally. Five different RDX-based propellant compositions have been formulated and the BURNING RATE and CALORIMETRIC VALUE were evaluated. The BURNING RATEs of RDX composite solid propellants increased with increasing RDX content. The data obtained from experimental tests indicates that increasing weight percentage of RDX in the formulation increases the pressure exponent and decreases the BURNING RATE constant. The mentioned parameters related to the propellant without RDX compared with other formulations including RDX. The results show that the BURNING RATE of the propellant without RDX at the constant pressure of 800Psi was 7.2 mm/s and as RDX content increased by 13.6%, the BURNING RATE decreased to 5.5 mm/s. The relationship between the BURNING RATE and RDX content was not linear. It was also found that the pressure exponent increased by increasing RDX content. As a result, the pressure exponent belonged to the based propellant was 0.22 that by increasing the percent of RDX to 13.6%, the pressure exponent increases up to 0.3.

Cites

No record.

References

No record.

Cite

APA: Copy

KARIMI, N., VAZIRI, S.A., & DEHNAVI, M.A.. (2015). EXPERIMENTAL INVESTIGATION OF BURNING RATE OF RDX/AP/AL/HTPB NITRAMINE PROPELLANTS. JOURNAL OF ENERGETIC MATERIALS, 9(3 (24)), 49-56. SID. https://sid.ir/paper/115446/en

Vancouver: Copy

KARIMI N., VAZIRI S.A., DEHNAVI M.A.. EXPERIMENTAL INVESTIGATION OF BURNING RATE OF RDX/AP/AL/HTPB NITRAMINE PROPELLANTS. JOURNAL OF ENERGETIC MATERIALS[Internet]. 2015;9(3 (24)):49-56. Available from: https://sid.ir/paper/115446/en

IEEE: Copy

N. KARIMI, S.A. VAZIRI, and M.A. DEHNAVI, “EXPERIMENTAL INVESTIGATION OF BURNING RATE OF RDX/AP/AL/HTPB NITRAMINE PROPELLANTS,” JOURNAL OF ENERGETIC MATERIALS, vol. 9, no. 3 (24), pp. 49–56, 2015, [Online]. Available: https://sid.ir/paper/115446/en

Related Journal Papers