Correlation between Alternating Temperature Accelerated Aging and Real World Storage of Composite Propellant

Author:

Ding Biao1,Shi Pei2,Qiu Xin1

Affiliation:

1. Naval Aeronautical and Astronautical University

2. Naval Aeronautical and Astronautical University

Abstract

Alternating temperature accelerated aging test was designed to ensure that accelerated aging could preferably simulate real world storage of HTPB composite propellant. Mechanical properties of HTPB propellant aged for three different periods were measured and analyzed. The results indicate that, the tensile strength increased and the elongation decreased after accelerated aging, showing the same trend of real world storage; the mechanical properties of HTPB propellant is strongly influenced by the rate of temperature change; alternating temperature accelerated aging test is consistent well with real world storage. The results can be very helpful for solid rocket motor life prediction.

Publisher

Trans Tech Publications, Ltd.

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference7 articles.

1. XU Xin-qi, YUAN Shu-sheng, SUI Yu-tang. Stress-strain analysis of propellant grains in storage[J]. Journal of Naval Aeronautical and Astronautical University, 2002, 17(3):313-317.

2. D Leveque, A Schieffer, A Mavel, et al Composites Science and Technology , 2005, 65: 395-401.

3. DONG Ke-hai. The evaluation method of remaining-life for charge of solid rocket motor based on cumulative damage[D]. Yantai:Naval Aeronautical and Astronautical University, (2007).

4. ZHANG Xing-gao. Study on the Aging Properties and Storage Life Prediction of HTPB Propellant[D]. Changsha:National University of Defense Technology, (2009).

5. Janajreh I, Heller R, Thangitham S Journal of Spacecraft and Rockets. 1994, 31(6): 1072-1078.

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