Real-Time Deep Throttling Tests of a Hydrogen Peroxide Hybrid Rocket Motor
Author:
Affiliation:
1. Technology for Propulsion and Innovation, 35129 Padova, Italy
2. University of Padova, 35131 Padova, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.B38504
Reference27 articles.
1. Dynamic Modeling of Hybrid Rocket Combustion
2. Time-Resolved Fuel-Grain Port Diameter Measurement in Hybrid Rockets
3. Modeling of Hybrid Rocket Low Frequency Instabilities
4. Numerical Model to Analyze Transient Behavior and Instabilities on Hybrid Rocket Motors
5. Investigation of Effect of Diaphragms on the Efficiency of Hybrid Rockets
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