Application of Nano‐Aluminum/Nitrocellulose Mesoparticles in Composite Solid Rocket Propellants-Reference-Cited by-同舟云学术

Application of Nano‐Aluminum/Nitrocellulose Mesoparticles in Composite Solid Rocket Propellants

Published:2015-04-16 Issue:3 Volume:40 Page:413-418
ISSN:0721-3115
Container-title:Propellants, Explosives, Pyrotechnics
language:en
Short-container-title:Propellants, Explosives, Pyrotechnics

Author:

Young Gregory¹,Wang Haiyang²,Zachariah Michael R.²

Affiliation:

1. RDT&E Department, Naval Surface Warfare Center Indian Head Explosive Ordnance Disposal Technology Division, Indian Head, MD 20640, USA

2. Department of Chemical and Biomolecular Engineering and Department of Chemistry and Biochemistry, University of Maryland, College Park, MD 20742, USA

Funder

Defense Threat Reduction Agency

Publisher

Wiley

Subject

General Chemical Engineering,General Chemistry

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1002/prep.201500020

Reference25 articles.

1. C. Zanotti A. Volpi M. Boanchessi L. De Luca Measuring Thermodynamic Properties of Burning Propellants in: Nonsteady Burning and Combustion Stability of Solid Propellants Vol. 143 Progress in Astronautics and Aeronautics 1992 AIAA Reston VA 145

2. E. W. Price R. K. Sigman Combustion of Aluminized Solid Propellants in: Solid Propellant Chemistry Combustion and Motor Interior Ballistics Vol. 185 Progress in Astronautics and Aeronautics 2000 AIAA Reston VA 663

3. Temperature of aluminum particles at the time of ignition and combustion

4. Ignition and combustion of aluminium particles in hot ambient gases

5. Combustion studies of single aluminum particles

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