Volume 11, Issue 1 (9-2015)                   مواد پرانرژی 2015, 11(1): 21-30 | Back to browse issues page

XML Persian Abstract Print


Download citation:
BibTeX | RIS | EndNote | Medlars | ProCite | Reference Manager | RefWorks
Send citation to:

molaei M, Moghiseh A, ferdosi M. مقایسه خواص شیمیایی و بالستیکی پیشرانه‌های کامپوزیتی اکسترود شده با حساسیت پایین با پیشرانه‌های بر پایه NG. مواد پرانرژی 2015; 11 (1) :21-30
URL: http://isaem.ir/article-1-761-en.html
, mmolaei75@yahoo.com
Abstract:   (4684 Views)

The enhancement of performance with a decrease in sensitivity of the propellant, have been considered in energetic materials research and development centers. Therefore, efforts to remove nitroglycerin from the common formulations while maintaining the efficiency of the propulsion system has been made, Which led to a new technology so called Extruded Composite Low Sensitive Propellant (ECL). This method reduces the sensitivity of the propellant and increases safety. The propellant ballistic efficiency increases due to increased bulk density and energy content, ascending combustion behavior and reduced temperature sensitivity. This paper is introduced ECL propellants and their chemical and ballistic properties, compared with conventional propellants.

Full-Text [PDF 1208 kb]   (1103 Downloads)    
Type of Study: T | Subject: پیشرانه
Published: 2016/02/2

Add your comments about this article : Your username or Email:
CAPTCHA

Send email to the article author


Rights and permissions
Creative Commons License This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License.

© 2024 CC BY-NC 4.0 | Iranian Scientific Association of Energetic Materials

Designed & Developed by : Yektaweb