Effect of Protrusion on Combustion Stability of Hybrid Rocket Motor
Author:
Affiliation:
1. Department of Space Engineering and Rocketry Birla Institute of Technology Mesra Ranchi 83215 India
Publisher
Wiley
Subject
General Chemical Engineering,General Chemistry
Link
https://onlinelibrary.wiley.com/doi/pdf/10.1002/prep.202100067
Reference48 articles.
1. D. Altman A. Holzman Overview and History of Hybrid Rocket Propulsion in: M. J. Chiaverini K. K. Kuo (Eds.) Fundamentals of Hybrid Rocket Combustion and Propulsion AIAA Progress in Astronautics and Aeronautics vol. 218 Inc. Raston VA 2006 p. 1–36.
2. G. P. Sutton O. Biblarz Classification in: Rocket Propulsion Elements Wiley New York 2000 p. 1–25.
3. K. K. Kuo M. Chiaverini Challenges of Hybrid Rocket Propulsion in the 21st Century in: M. J. Chiaverini K. K. Kuo (Eds.) Fundamentals of Hybrid Rocket Combustion and Propulsion AIAA Progress in Astronautics and Aeronautics vol. 218 Inc. Raston VA 2006 p. 593–638.
4. G. A. Risha B. J. Evans E. Boyer K. K. Kuo Metals Energetic Additives and Special Binders Used in Solid Fuels for Hybrid Rockets in: M. J. Chiaverini K. K. Kuo (Eds.) Fundamentals of Hybrid Rocket Combustion and Propulsion AIAA Progress in Astronautics and Aeronautics vol. 218 Inc. Raston VA 2006 p. 413–456.
5. Regression rates and burning characteristics of boron-loaded paraffin-wax solid fuels in ducted rocket applications
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