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Cited article:
L. Merotto , L. Galfetti , G. Colombo , L.T. DeLuca
Published online: 2012-10-01
This article has been cited by the following article(s):
6 articles
Combustion Characteristics of HTPB-Based Hybrid Rocket Fuels: Using Nickel Oxide as the Polymer Matrix Pyrolysis Catalyst
Hongsheng Yu, Xiaodong Yu, Hongwei Gao, Luigi T. DeLuca, Wei Zhang and Ruiqi Shen Aerospace 10 (9) 800 (2023) https://doi.org/10.3390/aerospace10090800
Innovative Energetic Materials: Properties, Combustion Performance and Application
Luigi T. DeLuca and WeiQiang Pang Innovative Energetic Materials: Properties, Combustion Performance and Application 111 (2020) https://doi.org/10.1007/978-981-15-4831-4_5
Effect of aluminum nanoparticles on rheological behavior of HTPB-based composite rocket propellant
Rohit Lade, Kailas Wasewar, Rekha Sangtyani, Arvind Kumar, Diwakar Shende and Dilip Peshwe Journal of Energetic Materials 37 (2) 125 (2019) https://doi.org/10.1080/07370652.2018.1543737
Enhancement of Solid Fuel Combustion in a Hybrid Rocket Motor Using Amorphous Ti–Al–B Nanopowder Additives
Terrence L. Connell, Richard A. Yetter, Grant A. Risha, et al. Journal of Propulsion and Power 35 (3) 662 (2019) https://doi.org/10.2514/1.B37330
Paraffin-based hybrid rocket engines applications: A review and a market perspective
Alessandro Mazzetti, Laura Merotto and Giordano Pinarello Acta Astronautica 126 286 (2016) https://doi.org/10.1016/j.actaastro.2016.04.036
An Italian network to improve hybrid rocket performance: Strategy and results
L. Galfetti, F. Nasuti, D. Pastrone and A.M. Russo Acta Astronautica 96 246 (2014) https://doi.org/10.1016/j.actaastro.2013.11.036