| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 11007132 | Vacuum | 2018 | 9 Pages |
Abstract
Modified iron oxide nanoparticles were synthesized via a simple co-precipitation method for their application as a burn rate modifier in composite solid propellant.389
Related Topics
Physical Sciences and Engineering
Materials Science
Surfaces, Coatings and Films
Authors
A.S. Budhwar, Aashish Gautam, Priyesh V. More, Chandra Shekhar Pant, Shaibal Banerjee, Pawan K. Khanna,