Metal–organic frameworks as hypergolic additives for hybrid rockets

Hybrid rocket propulsion can contribute to reduce launch costs by simplifying engine design and operation. Hypergolic propellants, i.e. igniting spontaneously and immediately upon contact between fuel and oxidizer, further simplify system integration by removing the need for an ignition system. Such...

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Detalles Bibliográficos
Autores principales: Jobin, Olivier, Mottillo, Cristina, Titi, Hatem M., Marrett, Joseph M., Arhangelskis, Mihails, Rogers, Robin D., Elzein, Bachar, Friščić, Tomislav, Robert, Étienne
Formato: Online Artículo Texto
Lenguaje:English
Publicado: The Royal Society of Chemistry 2022
Materias:
Chemistry
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8943900/
https://www.ncbi.nlm.nih.gov/pubmed/35432883
http://dx.doi.org/10.1039/d1sc05975k

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8943900/
https://www.ncbi.nlm.nih.gov/pubmed/35432883
http://dx.doi.org/10.1039/d1sc05975k

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