Service life prediction of AP/Al/HTPB solid rocket propellant with consideration of softening aging behavior

Author:

ADEL Walid M.,LIANG Guozhu

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference36 articles.

1. An investigation of composite propellant accelerated ageing mechanisms and kinetics;Judge;Propellants Explos Pyrotech,2003

2. Biggs GL. Solid propellant aging kinetics. 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit; 2009 Aug 2–5; Denver, Colorado. Reston: AIAA; 2009.p.1–13.

3. Mechanical and ballistic property variations of a solid propellant during accelerated ageing;Kadiresh;J Design Manuf Technol,2007

4. Huang WD, Xing YG. Mechanical property prediction method for a HTPB propellant aging. 43rd AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit; 2007 July 8-11; Cincinnati, USA. Reston: AIAA; 2007.p.1–5.

5. Mechanical properties of HTPB propellant after thermal accelerated aging and its life prediction;Wang;Chinese J Expl Propell,2015

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