A review on material characterization of composite solid propellant
Author:
Affiliation:
1. Department of Aerospace Engineering, Indian Institute of Technology Madras, Chennai, Tamil Nadu, India
Publisher
Informa UK Limited
Subject
Physics and Astronomy (miscellaneous)
Link
https://www.tandfonline.com/doi/pdf/10.1080/07370652.2023.2287466
Reference136 articles.
1. Investigation of Composite Solid Propellants Based on Nitrated Hydroxyl-Terminated Polybutadiene Binder
2. The use of the split Hopkinson pressure bar techniques in high strain rate materials testing
3. Epoxy composites based on glass beads. II. Mechanical properties
4. A predictive model for the mechanical behavior of particulate composites. Part I: Model derivation
5. Advances in science and technology of modern energetic materials: An overview
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