High-pressure burning rate studies of solid rocket propellants
Published online: 2013-03-05
Articles citing this article
The Citing articles tool gives a list of articles citing the current article.
The citing articles come from EDP Sciences database, as well as other publishers participating in CrossRef Cited-by Linking Program. You can set up your personal account to receive an email alert each time this article is cited by a new article (see the menu on the right-hand side of the abstract page).
Cited article:
This article has been cited by the following article(s):
Experimental investigation of solid propellants combustion response to pressure oscillations using advanced high-resolution diagnostics
Yu Liao, Bingning Jin, Siying Yang, Jiacheng Li, Peijin Liu and Yu GuanApplied Energy 377 124227 (2025)
https://doi.org/10.1016/j.apenergy.2024.124227
The regulation of ferrocene-based catalysts on heat transfer in high-pressure combustion of ammonium perchlorate/hydroxyl-terminated polybutadiene/aluminum composite propellants
Jinchao Han, Songqi Hu and Linlin LiuDefence Technology 35 174 (2024)
https://doi.org/10.1016/j.dt.2023.09.018
Catocene and Butacene Permanence as Ferrocenic Liquid Burning Rate Catalyst for Solid Composite Propellants and Comparison With Recent Developments
Javier Quagliano Amado, Rita C. L. Dutra, Jorge C. N. Dutra and Pablo RossPropellants, Explosives, Pyrotechnics (2024)
https://doi.org/10.1002/prep.202400190
Closed vessel burning rate measurements of composite propellants using microwave interferometry
Shane A. Oatman, August A. Caito, Daniel J. Klinger, James N. Cooper, Tim D. Manship and Steven F. SonPropellants, Explosives, Pyrotechnics 49 (8) (2024)
https://doi.org/10.1002/prep.202400072
Energetic hydrogen-bonded open-framework as promising green combustion catalyst for nitramine-based solid propellants
Lan Jiang, Hui Li, Ruibing Lv, Jinxing Wang, Siwei Song, Nan Sun, Michael Gozin, Kangcai Wang and Qinghua ZhangCombustion and Flame 257 113048 (2023)
https://doi.org/10.1016/j.combustflame.2023.113048
High-Pressure Combustion Characteristics of Hydroxyl-Terminated Polybutadiene Propellants
Jinchao Han, Songqi Hu, Linlin Liu and Pengxiang HeJournal of Propulsion and Power 1 (2022)
https://doi.org/10.2514/1.B38878
Isolating the effects of oxidizer characteristics and catalytic additives on the high-pressure exponent break of AP/HTPB-Composite propellants
Catherine A.M. Dillier, Erica D. Petersen and Eric L. PetersenProceedings of the Combustion Institute 38 (3) 4409 (2021)
https://doi.org/10.1016/j.proci.2020.08.008
Very-High-Pressure Burning Rates of Aluminized and Nonaluminized AP/HTPB-Composite Propellants
Catherine A. M. Dillier, Erica D. Petersen, Thomas Sammet and Eric L. PetersenJournal of Propulsion and Power 37 (5) 693 (2021)
https://doi.org/10.2514/1.B38173
Ballistics
Charles A. Osheku, Oluleke O. Babayomi and Oluwaseyi T. OlawoleBallistics (2019)
https://doi.org/10.5772/intechopen.82822
(2019)
https://doi.org/10.2514/6.2019-4368
Rare‐Earth Complexes with the 5,5′‐Bitetrazolate Ligand – Synthesis, Structure, Luminescence Properties, and Combustion Catalysis
Gleb A. Chesnokov, Maxim A. Topchiy, Andrey F. Asachenko, Nikita V. Muravyev, Leonid I. Grishin, Anna S. Nikiforova, Valentina V. Utochnikova, Victor B. Rybakov, Victor N. Khrustalev and Mikhail S. NechaevEuropean Journal of Inorganic Chemistry 2018 (6) 805 (2018)
https://doi.org/10.1002/ejic.201701154
Burning rate of AP/HTPB base-bleed composite propellant under free ambient pressure
Lingke Zhang, Ruyuan Tian and Zhuwei ZhangAerospace Science and Technology 62 31 (2017)
https://doi.org/10.1016/j.ast.2016.12.004
Ferrocene-based polyethyleneimines for burning rate catalysts
Zain-ul-Abdin Zain-ul-Abdin, Li Wang, Haojie Yu, et al.New Journal of Chemistry 40 (4) 3155 (2016)
https://doi.org/10.1039/C5NJ03171K
Integrated Fluid–Structure Simulation for Full Burning of a Solid-Propellant Rocket Interior
Sangho Han and Chongam KimJournal of Propulsion and Power 30 (4) 883 (2014)
https://doi.org/10.2514/1.B35107