Development of the Phoenix-1B Mk II 35 km Apogee Hybrid Rocket
Author:
Affiliation:
1. University of KwaZulu-Natal
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-4838
Reference13 articles.
1. Introduction to the University of KwaZulu-Natal Hybrid Sounding Rocket Program
2. An Integrated Six Degree-of-Freedom Trajectory Simulator for Hybrid Sounding Rockets
3. Performance Modeling of a Paraffin Wax / Nitrous Oxide Hybrid Rocket Motor
4. 4Geneviève, B. "Development of a Hybrid Sounding Rocket Motor," MSc Dissertation,Discipline of Mechanical Engineering, University of KwaZulu-Natal, Durban, 2013.
5. Flight Test of the Phoenix-1A Hybrid Rocket
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