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Validation with Numerical Simulations of a Simplified Model of a Hybrid Rocket Motor
Author(s) -
Frunzulica Florin,
StoiaDjeska Marius,
Mingireanu Florin
Publication year - 2015
Publication title -
pamm
Language(s) - English
Resource type - Journals
ISSN - 1617-7061
DOI - 10.1002/pamm.201510205
Subject(s) - aerospace engineering , impulse (physics) , specific impulse , propulsion , spacecraft propulsion , rocket (weapon) , work (physics) , computer science , mechanical engineering , engineering , physics , quantum mechanics
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 through numerical simulations a design tool for hybrid rocket motors (HRM). (© 2015 Wiley‐VCH Verlag GmbH & Co. KGaA, Weinheim)
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