Study on the Fracture Toughness of Hydroxyl-Terminated Polybutadiene Solid Rocket Propellant-Reference-Cited by-同舟云学术

Study on the Fracture Toughness of Hydroxyl-Terminated Polybutadiene Solid Rocket Propellant

Published:2015-05 Issue:3 Volume:31 Page:912-918
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Zhou Guangpan¹,Yin Xiaochun²,Li Aiqun¹

Affiliation:

1. School of Civil Engineering, Southeast University, 210096 Nanjing, People’s Republic of China

2. School of Science, Nanjing University of Science and Technology, 210094 Nanjing, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.B35467

Reference17 articles.

1. LeeJ. H. “Modeling of Crack Initiation and Growth in Solid Rocket Propellants Using Macromechanics and Micromechanics Theories,” M.S. Thesis, Naval Postgraduate School, Monterey, CA, 1996.

2. A study of loading history effect for thermoviscoelastic solid propellant grains

3. Fracture toughness of nitramine and composite solid propellants

4. J-integral resistance curve testing and evaluation

5. EverettR. A.Jr. “Review of Fatigue and Fracture Research at NASA Langley Research Center,” NASA Rept. N88-16633, 1988, pp. 535–572.

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