A Critical Analysis of Paraffin-based Fuel Formulations for Hybrid Rocket Propulsion
Author:
Affiliation:
1. Technical University of Milan
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-4830
Reference15 articles.
1. Vortex Combustion in a Lab-Scale Hybrid Rocket Motor
2. ANALYSIS OF QUASI-STEADY AND TRANSIENT BURNING OF HYBRID FUELS IN A LABORATORY-SCALE BURNER BY AN OPTICAL TECHNIQUE
3. TURBULENT BOUNDARY LAYER COMBUSTION IN THE HYBRID ROCKET
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