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Cited article:

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