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Nano-Sized and Mechanically Activated Composites: Perspectives for Enhanced Mass Burning Rate in Aluminized Solid Fuels for Hybrid Rocket Propulsion
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 [...]
MDPI and ACS Style

Carmicino, C. Special Issue “Advances in Hybrid Rocket Technology and Related Analysis Methodologies”. Aerospace 2019, 6, 128.

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