Nano Additives and Plateau Burning Rates of Ammonium-Perchlorate-Based Composite Solid Propellants
β Scribed by Stephens, Matthew A.; Petersen, Eric L.; Reid, David L.; Carro, Rodolphe; Seal, Sudipta
- Book ID
- 120391062
- Publisher
- American Institute of Aeronautics and Astronautics
- Year
- 2009
- Tongue
- English
- Weight
- 445 KB
- Volume
- 25
- Category
- Article
- ISSN
- 0748-4658
- DOI
- 10.2514/1.40831
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π SIMILAR VOLUMES
The burning rates of series of bi-and trimodal AP-HTPB propellants have been incorporated into an empirical statistical model which describes a hypothetical pentamodal polydisperse AP pseudopropellant. This pseudopropellant is the linear summation of five unimodal polydisperse AP pseudopropellants.
## Abstract The site and mechanism by which iron oxide catalyst acted to enhance burning rate and produced plateau burning behavior at high pressure was studied. The condensed phase chemistry study was conducted by isothermal thermogravimetric analysis (TGA) and differential scanning calorimetry (D