Enhanced Solid Fuel Regression in a Hybrid Rocket Employing Additively Manufactured Fuels Exhibiting Novel Grain Port Geometries
Author:
Affiliation:
1. Naval Surface Warfare Center
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2019-2015
Reference25 articles.
1. Turbulent boundary layer combustion in the hybrid rocket
2. Fundamentals of hybrid boundary layer combustion
3. Hybrid rocket development history
4. Schuler, A.L., Wiley, D. R. "Hybrid Propulsion Technology Program," Final Report No. GDSS-HPT89-001, 1989.
5. Combustion of Liquefying Hybrid Propellants: Part 1, General Theory
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