Review on the Dewetting of the Particle‐Matrix Interface in Composite Solid Propellants

Author:

Zou Zi‐Jie1,Qiang Hong‐Fu1,Li Yi‐Yi2,Wang Xue‐Ren1

Affiliation:

1. Zhijian laboratory Rocket Force University of Engineering Xi'an 710025 China

2. PLA of 96863 Luoyang 471003 China

Publisher

Wiley

Subject

General Chemical Engineering,General Chemistry

Reference132 articles.

1. Method for determining the tensile properties of solid rocket propellants CPIA Publish US 1957.

2. GJB770B-2005 Test method of propellant Commission of Science Technology and Industry for National Defense of PRC China 2005(in Chinese).

3. QJ2328A-2005 Test method for temperature accelerated aging of composite solid propellant Commission of Science Technology and Industry for National Defense of PRC China 2005(in Chinese).

4. Some aspects of nonlinear mechanical behavior of a composite propellant.

5. Mechanical Properties of Smokeless Composite Rocket Propellants Based on Prilled Ammonium Dinitramide

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