A Green Hybrid Thruster Using Moderately Enriched Compressed Air as the Oxidizer
Author:
Affiliation:
1. Utah State University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-4841
Reference17 articles.
1. Comparing Hydroxyl Terminated Polybutadiene and Acrylonitrile Butadiene Styrene as Hybrid Rocket Fuels
2. Development of a Power-Efficient, Restart-Capable Arc Ignitor for Hybrid Rockets
3. Survey of Selected Additively Manufactured Propellants for Arc Ignition of Hybrid Rockets
4. Effects of Radiation Heating on Additively Printed Hybrid Fuel Grain O/F Shift
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