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Conceptual Design of Hybrid Rocket

Evaluation module (cygwin script) for a launch vehicle (LV) with a hybrid rocket engine (HRE) is opened to the public. This module evaluates performances of designed LV with HRE and can be used as a real-world test problem for your optimizers and data mining techniques.
Please visit download and information site in our Wiki.

References

Kosugi, K., Oyama, A., Fujii, K., and Kanazaki, M., "Multidisciplinary and Multi-objective Design Exploration Methodology for Conceptual Design of a Hybrid Rocket," Infotech@aerospace2011, AIAA 2011-1634, 2011.

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