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