Tailoring of Mechanical Properties of Highly Filled Nano‐Aluminized Propellants by Modifying Binder Polymer Microstructure
Author:
Affiliation:
1. SF Complex, DRDO India
2. Department of Aerospace Engineering & National Centre for Combustion R&D Indian Institute of Technology Madras Chennai 600036 India
Publisher
Wiley
Subject
General Chemical Engineering,General Chemistry
Link
https://onlinelibrary.wiley.com/doi/pdf/10.1002/prep.202000182
Reference41 articles.
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3. Al2O3 collection and sizing from solid rocket motor plumes
4. Computer Model of Aluminum Agglomeration on Burning Surface of Composite Solid Propellant
5. L. T. DeLuca A. Bandera F. Maggi Agglomeration of Aluminized Solid Rocket Propellants 45thAIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit Denver Colorado USA August 2–5 2009 doi: https://doi.org/10.2514/6.2009-5439.
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