Combustion characteristics of cross-linked fluorinated polymer supported aluminum/oxidizer microsphere in HTPB propellant-Reference-Cited by-同舟云学术

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Combustion characteristics of cross-linked fluorinated polymer supported aluminum/oxidizer microsphere in HTPB propellant

Published:2022-03 Issue:1 Volume:2 Page:20-27
ISSN:2667-1344
Container-title:FirePhysChem
language:en
Short-container-title:FirePhysChem

Author:

Zhang Tianfu,Yao Nan,Zhou Chongyang,Li Yang,Zhao Yanpeng,Pang Aimin,Wu Shixi

Publisher

Elsevier BV

Subject

General Earth and Planetary Sciences,General Environmental Science

Reference27 articles.

1. Chemical Rocket Propulsion: A Comprehensive Survey of Energetic Materials;DeLuca,2017

2. Combustion efficiency of aluminized propellant;Suzuki,1989

3. Role of pressure and aluminum size in solid propellant CCP generation;Maggi,2017

4. A pocket model for aluminum agglomeration in composite propellants;Cohen;AIAA J.,1983

5. Pocket model for aluminum agglomeration based on propellant microstructure;Maggi;AIAA J.,2015

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1. Surface-Hydrophobic Al@COFs Core-Shell structured Composites: A class of efficient high-energy fuels;Fuel;2024-09

2. Combustion performance modulation and agglomeration inhibition of HTPB propellants by fine Al/oxidizers integration;Fuel;2024-07

3. Research progress and prospects on agglomeration models and simulation methods of aluminum particles in aluminum‐based composite propellants;Propellants, Explosives, Pyrotechnics;2024-06-21

4. Citric acid enhances the ignition and combustion performance of aluminum: Coating and etching;Colloids and Surfaces A: Physicochemical and Engineering Aspects;2024-05

5. Low-temperature ignition and mechanism of μAl coated with bismuth citrate;Combustion and Flame;2023-12

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