Exploring Mechanisms of Particle Size Effects of Iron Oxide on Thermal Behaviors and Combustion Characteristics for 5AT/Sr(NO3)2 Propellant
Author:
Affiliation:
1. University of Science and Technology of China
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-4427
Reference23 articles.
1. A Modeling Investigation of Suppressant Distribution from a Prototype Solid-Propellant Gas-Generator Suppression System into a Simulated Aircraft Cargo Bay
2. Burning Characteristics and Sensitivity Characteristics of Some Guanidinium 1,5′-bis -1H-Tetrazolate/Metal Oxide Mixtures as Candidate Gas Generating Agent
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