Energetic Nanocomposites as Burn Rate Catalyst for Composite Solid Propellants-Reference-Cited by-同舟云学术

Energetic Nanocomposites as Burn Rate Catalyst for Composite Solid Propellants

Published:2017-11-28 Issue:2 Volume:43 Page:136-143
ISSN:0721-3115
Container-title:Propellants, Explosives, Pyrotechnics
language:en
Short-container-title:Prop., Explos., Pyrotech.

Author:

Bagalkote Vrushali¹,Grinstein Dan²,Natan Benveniste³

Affiliation:

1. Postdoctoral Research Fellow, Sylvia and David I.A. Fine Rocket Propulsion Center, Faculty of Aerospace EngineeringTechnion-Israel Institute of Technology Haifa 32000 Israel

2. Scientific AdvisorTechnion-Israel Institute of Technology Haifa 32000 Israel

3. Steven Berger Professor Chair of Engineering, Head of Sylvia and David I.A. Fine Rocket Propulsion Center, Faculty of Aerospace EngineeringTechnion-Israel Institute of Technology Haifa 32000 Israel

Funder

PBC Program for Fellowships

Publisher

Wiley

Subject

General Chemical Engineering,General Chemistry

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1002/prep.201700095

Reference32 articles.

1. A. Dokhan E. W. Price J. M. Seitzman R. K. Sigman The Ignition of Ultra-Fine Aluminum in Ammonium Perchlorate Solid Propellant Flames 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit AIAA 2003-4810 July2003.

2. N. Kubota Thermochemical Aspects of Combustion Wiley-VCH Weinheim2002 p. 158.

3. M. Kohga Burning Characteristics and Thermochemical Behavior of AP/HTPB Composite Propellant Using Coarse and Fine AP Particles Propellants Explos. Pyrotech.2011 36 57–64.