Special Issue “Advances in Hybrid Rocket Technology and Related Analysis Methodologies”
Department of Industrial Engineering—Aerospace Division, University of Naples “Federico II”, Piazzale Tecchio, 80-80125 Naples, Italy
Aerospace 2019, 6(12), 128; https://doi.org/10.3390/aerospace6120128
Received: 21 November 2019 / Accepted: 21 November 2019 / Published: 26 November 2019
(This article belongs to the Special Issue Advances in Hybrid Rocket Technology and Related Analysis Methodologies)
Note: In lieu of an abstract, this is an excerpt from the first page.
Hybrid rockets are chemical propulsion systems that, in the most common configuration, employ a liquid oxidizer (or gaseous in much rarer cases) and a solid fuel; the oxidizer, stored in tanks, is properly injected in the combustion chamber where the solid fuel grain is bonded [...] View Full-Text
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MDPI and ACS Style
Carmicino, C. Special Issue “Advances in Hybrid Rocket Technology and Related Analysis Methodologies”. Aerospace 2019, 6, 128. https://doi.org/10.3390/aerospace6120128
AMA Style
Carmicino C. Special Issue “Advances in Hybrid Rocket Technology and Related Analysis Methodologies”. Aerospace. 2019; 6(12):128. https://doi.org/10.3390/aerospace6120128
Chicago/Turabian StyleCarmicino, Carmine. 2019. "Special Issue “Advances in Hybrid Rocket Technology and Related Analysis Methodologies”" Aerospace 6, no. 12: 128. https://doi.org/10.3390/aerospace6120128
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