Works matching DE "SOLID propellants"
Results: 733
Numerical Simulation of the Gas Flow of Combustion Products from Ignition in a Solid Rocket Motor Under Conditions of Propellant Creep.
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- Aerospace (MDPI Publishing), 2025, v. 12, n. 2, p. 153, doi. 10.3390/aerospace12020153
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Decomposition Reaction Mechanism of Ammonium Perchlorate on N-Doped Graphene Surfaces: A Density Functional Theory Study.
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- Molecules, 2025, v. 30, n. 4, p. 837, doi. 10.3390/molecules30040837
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Comparative Study on Extrusion 3D Printing of Solid Propellant Based on Plunger and Screw.
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- Materials (1996-1944), 2025, v. 18, n. 4, p. 777, doi. 10.3390/ma18040777
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Research on Curing Reaction Kinetics and Curing Process of Nitrate Ester Plasticized Polyether (NEPE) Propellants.
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- Polymers (20734360), 2025, v. 17, n. 4, p. 464, doi. 10.3390/polym17040464
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Vibrational Spectroscopic Studies of Alane.
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- Journal of Energetic Materials, 2005, v. 23, n. 3, p. 169, doi. 10.1080/07370650591001844
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Burning Rate Studies of Metal Powder (Ti, Ni)–Based Fuel-Rich Propellants.
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- Journal of Energetic Materials, 2004, v. 22, n. 2, p. 55, doi. 10.1080/07370650490492770
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Synthesis, Characterization and Energetic Properties of Hydroxymethyl‐Bishomocubanone Derivatives.
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- Chemistry - A European Journal, 2024, v. 30, n. 47, p. 1, doi. 10.1002/chem.202401265
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Effects of Nano-Nickel Oxide on Thermokinetics, Thermal Safety, and Gas-Generating Characteristics of 5-Aminotetrazole Thermal Degradation.
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- Fire (2571-6255), 2023, v. 6, n. 4, p. 172, doi. 10.3390/fire6040172
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Launching to an orbit with a chemical propellant staged rocket systems.
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- Manas Journal of Engineering, 2022, v. 10, n. 1, p. 42, doi. 10.51354/mjen.1000248
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Application of Reconstruction of Variational Iteration Method on the Laminar Flow in a Porous Cylinder with Regressing Walls.
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- Mechanics & Mechanical Engineering, 2017, v. 21, n. 2, p. 379
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Three-Dimensional Numerical Modeling of Internal Ballistics for Solid Propellant Combinations.
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- Mathematics (2227-7390), 2021, v. 9, n. 21, p. 2714, doi. 10.3390/math9212714
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Performance Evaluation of Combustion-controllable 0.1-N-Class Solid Propellant Microthrusters Using Laser Heating.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2021, v. 64, n. 2, p. 65, doi. 10.2322/tjsass.64.65
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Experimental Investigation of a Solid Propellant Ducted Rocket with a Chin Type Inlet.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2019, v. 62, n. 5, p. 284, doi. 10.2322/tjsass.62.284
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Characterization of a Liquid-propellant Pulsed Plasma ThrusterUsing Various Nozzle Configurations.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2019, v. 62, n. 4, p. 184, doi. 10.2322/tjsass.62.184
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Microstructure and interaction in aluminum hydrides@polydopamine composites and interfacial improvement with GAP adhesive.
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- Scientific Reports, 2024, v. 14, n. 1, p. 1, doi. 10.1038/s41598-024-59944-1
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SÍNTESE DO CROMITO DE COBRE (II).
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- Periódico Tchê Química, 2013, v. 10, n. 19, p. 30, doi. 10.52571/ptq.v10.n19.2013.30_periodico19_pgs_30_37.pdf
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Review of novel energetic polymers and binders – high energy propellant ingredients for the new space race.
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- Designed Monomers & Polymers, 2019, v. 22, n. 1, p. 54, doi. 10.1080/15685551.2019.1575652
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Thixotropic Behavior in Defining Particle Packing Density of Highly Filled AP/HTPB-Based Propellant.
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- Symmetry (20738994), 2021, v. 13, n. 10, p. 1767, doi. 10.3390/sym13101767
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Analysis of thermal radiation from burning aluminium in solid propellants.
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- Combustion Theory & Modelling, 2009, v. 13, n. 3, p. 389, doi. 10.1080/13647830802684318
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Limitation of the ZN approach for calculating the response function of homogeneous propellants.
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- Combustion Theory & Modelling, 2008, v. 12, n. 6, p. 1049, doi. 10.1080/13647830802203846
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The three-dimensional numerical simulation of aluminized composite solid propellant combustion.
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- Combustion Theory & Modelling, 2008, v. 12, n. 1, p. 45, doi. 10.1080/13647830701395099
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Application of continuation techniques to ammonium perchlorate plane flames.
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- Combustion Theory & Modelling, 2006, v. 10, n. 5, p. 771, doi. 10.1080/13647830500485133
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Particle packing models to determine time-dependent slip flow properties of highly filled polyurethane-based propellant.
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- Journal of Rubber Research, 2022, v. 25, n. 2, p. 157, doi. 10.1007/s42464-022-00166-3
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Structural Behavior Examination of Frequently Used Solid Propellant Sections Under Centrifugal Loading Using Response Surface Method.
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- Journal of Aeronautics & Space Technologies / Havacilik ve Uzay Teknolojileri Dergisi, 2021, v. 14, n. 2, p. 231
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Targets in Combat: Hats off to the BQM-34 Firebee.
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- Wings of Gold, 2019, v. 44, n. 2, p. 22
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- Article
Fracture behaviour of accelerated aged solid rocket propellants.
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- Journal of Materials Science, 1999, v. 34, n. 17, p. 4209, doi. 10.1023/A:1004690416667
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Ultrasonic Tomographic Imaging of an Encased, Highly Attenuating Solid Medium.
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- Research in Nondestructive Evaluation, 2001, v. 13, n. 3, p. 131, doi. 10.1080/09349840109409693
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A Modeling Investigation of Suppressant Distribution from a Prototype Solid-Propellant Gas-Generator Suppression System into a Simulated Aircraft Cargo Bay.
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- Drying Technology, 2007, v. 25, n. 6, p. 1021, doi. 10.1080/07373930701396410
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基于人工神经网络的固体推进剂细观损伤与 宏观刚度映射关系.
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- Acta Materiae Compositae Sinica, 2024, v. 41, n. 9, p. 4765, doi. 10.13801/j.cnki.fhclxb.20240423.003
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细观结构参量对推进剂力学性能影响的 数值研究.
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- Acta Materiae Compositae Sinica, 2022, v. 39, n. 6, p. 2949, doi. 10.13801/j.cnki.fhclxb.20210708.001
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一种高颗粒填充率丁羟推进剂二维细观模型 生成方法.
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- Acta Materiae Compositae Sinica, 2019, v. 36, n. 10, p. 2302, doi. 10.13801/j.cnki.fhclxb.20190221.001
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基于固体火箭发动机工作原理的两种推进剂燃速测试方法对比.
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- Chinese Journal of Explosives & Propellants, 2024, v. 47, n. 11, p. 1031, doi. 10.14077/j.issn.1007-7812.202401009
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HTPE 固体推进剂点火能量和燃烧特性的实验研究.
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- Chinese Journal of Explosives & Propellants, 2024, v. 47, n. 11, p. 1022, doi. 10.14077/j.issn.1007-7812.202403026
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复合固体推进剂药浆浇铸工艺仿真及优化.
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- Chinese Journal of Explosives & Propellants, 2024, v. 47, n. 10, p. 937, doi. 10.14077/j.issn.1007-7812.202309006
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固体推进剂断裂与裂纹扩展研究进展.
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- Chinese Journal of Explosives & Propellants, 2024, v. 47, n. 10, p. 857, doi. 10.14077/j.issn.1007-7812.202308011
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- Article
Thermal Induced Damage Evolution of GAP/AP/RDX/A1 Composite Solid Propellant.
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- Chinese Journal of Explosives & Propellants, 2024, v. 47, n. 9, p. 840, doi. 10.14077/j.issn.1007-7812.202403025
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Effect of Strain Rate on Mechanical Properties and Failure Mechanisms of HTPB Propellant with High Solid Content.
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- Chinese Journal of Explosives & Propellants, 2024, v. 47, n. 7, p. 656, doi. 10.14077/j.issn.1007-7812.202316010
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Effect of Strain Rate on Mechanical Properties and Failure Mechanisms of HTPB Propellant with High Solid Content.
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- Chinese Journal of Explosives & Propellants, 2024, v. 47, n. 7, p. 656, doi. 10.14077/j.issn.1007-7812.202319010
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Synthesis and Property Characterization of New Schiff Base Bonding Agent for Solid Propellant.
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- Chinese Journal of Explosives & Propellants, 2024, v. 47, n. 7, p. 649, doi. 10.14077/j.issn.1007-7812.202310007
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Catalytic Effect of Transition Metal Complexes of Triaminoguanidine on the Thermolysis of Energetic NC/DEGDN Composite.
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- Chinese Journal of Explosives & Propellants, 2024, v. 47, n. 3, p. 209, doi. 10.14077/j.issn.1007-7812.202312007
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Research Progress on Meso-damage Evolution of Composite Solid Propellants.
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- Chinese Journal of Explosives & Propellants, 2023, v. 46, n. 12, p. 1043, doi. 10.14077/j.issn.1007-7812.202303001
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一种高能固体推进剂定压燃烧温度的确定方法.
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- Chinese Journal of Explosives & Propellants, 2023, v. 46, n. 9, p. 840, doi. 10.14077/j.issn.1007-7812.202212007
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复合固体推进剂强度、损伤与断裂失效研究进展.
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- Chinese Journal of Explosives & Propellants, 2023, v. 46, n. 7, p. 561, doi. 10.14077/j.issn.1007-7812.202211020
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纳米碳材料基复合燃烧催化剂的应用研究进展.
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- Chinese Journal of Explosives & Propellants, 2023, v. 46, n. 7, p. 589, doi. 10.14077/j.issn.1007-7812.202212009
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二茂铁月青氧化物的合成及其催化和抗迁移性能.
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- Chinese Journal of Explosives & Propellants, 2023, v. 46, n. 3, p. 229, doi. 10.14077/j.issn.1007-7812.202211014
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Research Progress of Al-based Alloy Fuels and Perspectives for Applications in Solid Propellants.
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- Chinese Journal of Explosives & Propellants, 2023, v. 46, n. 2, p. 101, doi. 10.14077/j.issn.1007-7812.202203029
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- Article
Study on the Combustion Characteristics of Al/AP/HTTP Propellant Based on High-speed Off-axis Holographic Visualization.
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- Chinese Journal of Explosives & Propellants, 2023, v. 46, n. 2, p. 179, doi. 10.14077/j.issn.1007-7812.202209010
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低聚硅倍半氧烷在HTPB复合推进剂中的多功能作用.
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- Chinese Journal of Explosives & Propellants, 2023, v. 46, n. 1, p. 76, doi. 10.14077/j.issn.1007-7812.202206006
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固体推进剂含能燃烧催化剂研究现状与发展趋势.
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- Chinese Journal of Explosives & Propellants, 2023, v. 46, n. 1, p. 1, doi. 10.14077/j.issn.1007-7812.202204001
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Creep Properties of GAP-ETPE-based High-energy Solid Propellant.
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- Chinese Journal of Explosives & Propellants, 2022, v. 45, n. 6, p. 877, doi. 10.14077/j.issn.1007-7812.202208005
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