Patent · US Active

Burn rate sensitization of solid propellants using a nano-titania additive

US8066834B1 · kind B1 · utility

6Cited by
12References
7Claims
0Family size

Assignee

Inventors

Key dates

Filing dateAug 3, 2006
Grant dateNov 29, 2011
Priority date
Expiry dateNov 11, 2028

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10S149/11
  • WIPO fieldMaterials, metallurgy
  • WIPO sectorChemistry

Abstract

Adding nanoparticles as a catalyst to solid propellant fuel to increase and enhance burn rates of the fuel by up to 10 times or more and/or modifying the pressure index. A preferred embodiment uses TiO2 nanoparticles mixed with a solid propellant fuel, where the nanoparticles are approximately 2% or less of total propellant mixture. The high surface to volume ratio of the nanoparticles improve the performance of the solid propellant fuel.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.