Effects of grain size and temperature of double base solid propellants on internal ballistics performance

Author:

Degirmenci Ercan

Publisher

Elsevier BV

Subject

Organic Chemistry,Energy Engineering and Power Technology,Fuel Technology,General Chemical Engineering

Reference11 articles.

1. http://www.nakka-rocketry.net/burnrate.html.

2. AMCP 706-247 Ammunition Series, Section 4, Design for Projection, Headquarters, U.S. Army Materiel Command; July 1964.

3. Sutton GP. Rocket propulsion elements, 7th ed., USA; 2010. ISBN 978-0-471-08024-5.

4. A thermochemical approach for the determination of convection heat transfer coefficients in a gun barrel;Degirmenci;Appl Therm Eng,2012

5. Kubato N. Propellant and explosives. Germany; 2002. ISBN: 3-527-30210-7.

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