Ferrocene-fullerene dyad as a novel burn rate modifier for propellants

The burn rate of composite rocket propellants serves as a critical ballistic parameter in the construction of a rocket engine. Due to their large surface areas, carbon-based materials such as carbon nanotubes, graphene, and fullerene have demonstrated promising results as burn rate modifiers (BRMs)...

Cur síos iomlán

Sonraí bibleagrafaíochta
Príomhchruthaitheoirí: Shrutika Sriramrao, Parveen Raman, Akash Dhas, Shaibal Banerjee
Formáid: Alt
Teanga:English
Foilsithe / Cruthaithe: KeAi Communications Co. Ltd. 2024-03-01
Sraith:Energetic Materials Frontiers
Ábhair:
Rochtain ar líne:http://www.sciencedirect.com/science/article/pii/S2666647224000022