Numerical Simulations of Flow and Fuel Regression Rate Coupling in Hybrid Rocket Motors
Journal Title: INCAS BULLETIN - Year 2017, Vol 9, Issue 1
Abstract
The hybrid propulsion offers some remarkable advantages like high safety and high specific impulse and thus it is considered a promising technology for the next generation launchers and space systems. The purpose of this work is to validate a design tool for hybrid rocket motors (HRM) through numerical simulations.
Authors and Affiliations
Marius STOIA-DJESKA STOIA-DJESKA, Florin FRUNZULICA
Keywords
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- EP ID EP293088
- DOI 10.13111/2066-8201.2017.9.1.9
- Views 111
- Downloads 0
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