Effect of fluorinated graphite on combustion of boron and boron-based fuel-rich propellants
Author:
Affiliation:
1. Chung Shan Institute of Science and Technology, Lungtan, Taiwan 32526, Republic of China
2. Chung Cheng Institute of Technology, Tashi, Taiwan 33509, Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.23986
Reference14 articles.
1. Advantages and drawbacks of boron-fueled propulsion
2. Effect of Boron Particle Surface Coating on combustion of solid propellants for ducted rockets
3. Combustion characteristics of GAP-coated boron particles and the fuel-rich solid propellant
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