Generating Plateau Burning Segments for Composite Solid Rocket Propellants
Author:
Affiliation:
1. Military Technical College 11766 Kobry El-Kobba Cairo Egypt
2. Department of Chemical EngineeringThe British University in Egypt 11837 El-Sherouk City Cairo Egypt
Funder
Cairo University, Egypt
Military Technical College, Egypt
Publisher
Wiley
Subject
General Chemical Engineering,General Chemistry
Link
https://onlinelibrary.wiley.com/doi/pdf/10.1002/prep.201900138
Reference39 articles.
1. High Energy Materials
2. K. Klager G. A. Zimmerman Steady Burning Rate and Affecting Factors: Experimental Results in: L. De Luca E. W. Price and M. Summerfield Nonsteady Burning and Combustion Stability of Solid Propellants Vol 143 American Institute of Aeronautics and Astronautics Washington 1992 pp. 59–109.
3. N. Kubota Survey of Rocket Propellants and Their Combustion Characteristics in: K. K. Kuo M. Summerfield Fundamentals of Solid-Propellant Combustion Progress in astronautics and aeronautics Vol 90 American Institute of Aeronautics and Astronautics Washington 1984 pp. 1–52.
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