HTPB‐Clay Nanocomposites (HCN): An Efficient Burning Rate Catalyst for Composite Propellant
Author:
Affiliation:
1. High Energy Materials Research Laboratory, Sutarwadi Pune- 411021 India
2. Defence Institute of Advanced Technology, Girinagar Pune- 411025 India
Funder
Shri K P S Murthy, Director, HEMRL
Publisher
Wiley
Subject
General Chemical Engineering,General Chemistry
Link
https://onlinelibrary.wiley.com/doi/pdf/10.1002/prep.201800333
Reference34 articles.
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3. M. W.Beckstead An Overview of combustion Mechanics and Flame Structures for Advanced Solid Propellants Solid Propellant Chemistry Combustion and Motor Interior Ballistics(Eds.: V. Yang T. Brill W. Ren) Progress in Astronautics and Aeronautics AIAA Vol.185 New York2000 267.
4. K. Kishore V. Gayathri Chemistry of Ignition and Combustion of Ammonium Perchlorate-Based Propellants in:Fundamentals of solid Propellant Combustion(Eds.: K. K.Kuo M. Summerfield) Progress in Astronautics and Aeronautics AIAA Vol. 90 New York1984 53.
5. K. Ramohalli Steady State Burning of Composite Propellants Under Zero Cross-Flow Situation Fundamentals of Solid-Propellant Combustion Progress in Astronautics and Aeronautics AIAA Vol. 90 New York1984 409.
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