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Open AccessEditorial

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
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
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 Style

Carmicino, 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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Note that from the first issue of 2016, MDPI journals use article numbers instead of page numbers. See further details here.

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