Works matching DE "SOLID propellants"
Results: 743
Solid propellants burning enhancement using foil embedding method.
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- Aeronautical Journal, 2008, v. 112, n. 1138, p. 725, doi. 10.1017/S0001924000002694
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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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Molecular dynamics research on interfacial reinforcement between ε-CL-20 and polymeric bonding agents for humidity-insensitive solid propellant systems.
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- Journal of Polymer Research, 2021, v. 28, n. 6, p. 1, doi. 10.1007/s10965-021-02571-5
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Alkynyl-functionalization of carbon nanotubes to promote anchoring potential in glycidyl azide polymer-based binders via Huisgen reaction for solid propellant application.
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- Journal of Polymer Research, 2021, v. 28, n. 4, p. 1, doi. 10.1007/s10965-021-02468-3
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Thermodynamic properties of polyvinyl alcohol binder of electrically controlled solid propellant.
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- Journal of Polymer Research, 2019, v. 26, n. 9, p. N.PAG, doi. 10.1007/s10965-019-1894-2
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A quasi-dynamic procedure for coupled thermal simulations.
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- International Journal for Numerical Methods in Fluids, 2013, v. 72, n. 11, p. 1183, doi. 10.1002/fld.3782
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Investigation of thermomechanical properties of solid rocket propellant used in multi-barrel rocket systems.
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- Continuum Mechanics & Thermodynamics, 2024, v. 36, n. 3, p. 459, doi. 10.1007/s00161-023-01277-x
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Nonlinear analysis for propellant solids.
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- Continuum Mechanics & Thermodynamics, 2022, v. 34, n. 5, p. 1159, doi. 10.1007/s00161-022-01111-w
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Energy Potential of Zwitterionic Nitrohydrazine As a Component of Solid Composite Propellants.
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- Combustion, Explosion, & Shock Waves, 2024, v. 60, n. 3, p. 318, doi. 10.1134/S0010508224030055
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Burning Characteristics in a Wide Range of Pressure and Thermal Decomposition of AP/PBT Solid Propellants.
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- Combustion, Explosion, & Shock Waves, 2023, v. 59, n. 6, p. 759, doi. 10.1134/S0010508223060126
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Pocket Model with a Tetrahedral Cell for Aluminum Agglomeration in Composite Propellants.
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- Combustion, Explosion, & Shock Waves, 2023, v. 59, n. 6, p. 752, doi. 10.1134/S0010508223060114
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Combustion Characteristics of High-Energy Material Containing Dispersed Aluminum, Boron, and Aluminum Borides.
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- Combustion, Explosion, & Shock Waves, 2023, v. 59, n. 4, p. 440, doi. 10.1134/S0010508223040068
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Pasty Propellants and Features of Their Burning.
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- Combustion, Explosion, & Shock Waves, 2023, v. 59, n. 2, p. 236, doi. 10.1134/S0010508223020156
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Excessive Subsurface Heat Release As a Possible Cause of the Negative Erosion Effect during Combustion of Homogeneous Solid Propellants.
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- Combustion, Explosion, & Shock Waves, 2022, v. 58, n. 6, p. 638, doi. 10.1134/S0010508222060028
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Combustion of a Composite Solid Propellant with Addition of Boron Powder.
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- Combustion, Explosion, & Shock Waves, 2022, v. 58, n. 5, p. 602, doi. 10.1134/S0010508222050136
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Laser Ignition of Aluminum and Boron Based Powder Systems.
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- Combustion, Explosion, & Shock Waves, 2022, v. 58, n. 4, p. 422, doi. 10.1134/S0010508222040049
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Intermediate Structures in the Process of Burning of High-Energy Condensed Systems.
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- Combustion, Explosion, & Shock Waves, 2022, v. 58, n. 4, p. 408, doi. 10.1134/S0010508222040025
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Combustion Model for a Composite Solid Propellant with an Evaporating Coolant.
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- Combustion, Explosion, & Shock Waves, 2022, v. 58, n. 3, p. 362, doi. 10.1134/S0010508222030121
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Numerical Simulation of Combustion of a Composite Solid Propellant Containing Boron Powder.
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- Combustion, Explosion, & Shock Waves, 2022, v. 58, n. 2, p. 197, doi. 10.1134/S0010508222020095
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Effect of Particle Orientation on the Burning Rate of Ammonium-Perchlorate-Based Solid Propellants.
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- Combustion, Explosion, & Shock Waves, 2021, v. 57, n. 6, p. 685, doi. 10.1134/S0010508221060071
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Prospects of Using Boron Powders As Fuel. III. Influence of Polymer Binders on the Composition of Condensed Gasification Products of Model Boron-Containing Compositions.
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- Combustion, Explosion, & Shock Waves, 2021, v. 57, n. 5, p. 547, doi. 10.1134/S001050822105004X
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Investigation of Acoustic Instability in Solid-Propellant Rocket Motors with the Use of a Pulsed T-Burner.
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- Combustion, Explosion, & Shock Waves, 2021, v. 57, n. 4, p. 433, doi. 10.1134/S0010508221040067
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Modeling of Ignition and Combustion of Boron-Containing Solid Propellants.
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- Combustion, Explosion, & Shock Waves, 2021, v. 57, n. 3, p. 308, doi. 10.1134/S0010508221030059
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Thermochemical and Energy Characteristics of Dimers of Terfurazanoazepines.
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- Combustion, Explosion, & Shock Waves, 2020, v. 56, n. 6, p. 621, doi. 10.1134/S0010508220060015
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Thermochemical and Energy Characteristics of N-(2,2-bis(methoxy-NNO-azoxy)ethyl)nitramines.
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- Combustion, Explosion, & Shock Waves, 2020, v. 56, n. 4, p. 464, doi. 10.1134/S0010508220040103
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On the Effectiveness of Using the Real Law of Solid Propellant Burning Rate As a Function of Solid Rocket Motor Pressure.
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- Combustion, Explosion, & Shock Waves, 2020, v. 56, n. 2, p. 172, doi. 10.1134/S0010508220020082
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Prospects of Using Boron Powders As Fuel. II. Influence of Aluminum and Magnesium Additives and Their Compounds on the Thermal Behavior of Boron Oxide.
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- Combustion, Explosion, & Shock Waves, 2020, v. 56, n. 2, p. 148, doi. 10.1134/S0010508220020057
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Evaluation of the Performance of Some Metals and Nonmetals in Solid Propellants for Rocket-Ramjet Engines.
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- Combustion, Explosion, & Shock Waves, 2020, v. 56, n. 1, p. 71, doi. 10.1134/S0010508220010098
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Thermodynamic Estimate of the Optimal Ratio of the Solid Propellant and Fuel in the Gas Generator of a High-Velocity Flying Vehicle.
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- Combustion, Explosion, & Shock Waves, 2019, v. 55, n. 6, p. 702, doi. 10.1134/S001050821906011X
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Combustion Hotspots of Energetic Condensed Systems.
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- Combustion, Explosion, & Shock Waves, 2019, v. 55, n. 6, p. 661, doi. 10.1134/S0010508219060054
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Thermochemical and Energy Characteristics of Alkoxy-NNO-Azoxy Derivatives of Pyrazole and Nitropyrazoles.
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- Combustion, Explosion, & Shock Waves, 2019, v. 55, n. 3, p. 327, doi. 10.1134/S0010508219030109
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Thermochemical and Energy Characteristics of DAzFF and AzNTF.
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- Combustion, Explosion, & Shock Waves, 2019, v. 55, n. 2, p. 148, doi. 10.1134/S0010508219020035
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Energy Potential of Some Hypothetical Derivatives of Tetrazole as Components of Solid Composite Propellants.
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- Combustion, Explosion, & Shock Waves, 2019, v. 55, n. 1, p. 32, doi. 10.1134/S0010508219010040
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Thermochemical and Energy Characteristics Di-, Tri-, and Tetra-Azido-Substituted Azines As Gasifying Agents of Solid Fuels for Ramjet Engines.
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- Combustion, Explosion, & Shock Waves, 2019, v. 55, n. 1, p. 23, doi. 10.1134/S0010508219010039
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Diffusion Model of Combustion of Large Boron Particles.
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- Combustion, Explosion, & Shock Waves, 2018, v. 54, n. 4, p. 442, doi. 10.1134/S0010508218040081
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Performance optimization of a standard-flow hybrid rocket engine.
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- Combustion, Explosion, & Shock Waves, 2017, v. 53, n. 6, p. 634, doi. 10.1134/S001050821706003X
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Determination of the transfer coefficients of natural turbulence occurring near the solid-propellant gasification zone. II. hydrodynamic instability in the presence of cross-flow.
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- Combustion, Explosion, & Shock Waves, 2017, v. 53, n. 6, p. 641, doi. 10.1134/S0010508217060041
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Effect of distributed injection of air into the afterburning chamber of a ram-rocket engine on the efficiency of combustion of boron particles.
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- Combustion, Explosion, & Shock Waves, 2017, v. 53, n. 6, p. 652, doi. 10.1134/S0010508217060053
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Determination of the transfer coefficient of natural turbulence occurring near the solid-propellant gasification zone. I. Two-phase model of the gasification zone.
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- Combustion, Explosion, & Shock Waves, 2017, v. 53, n. 5, p. 554, doi. 10.1134/S0010508217050082
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Molecular beam mass spectrometry of solid propellant combustion products at a pressure of 40 atm.
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- Combustion, Explosion, & Shock Waves, 2017, v. 53, n. 5, p. 565, doi. 10.1134/S0010508217050094
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Calculation of pressure in a solid-propellant rocket motor with the use of a real dependence of the solid propellant burning rate on pressure.
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- Combustion, Explosion, & Shock Waves, 2017, v. 53, n. 5, p. 569, doi. 10.1134/S0010508217050100
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Study of a hybrid gas generator for a ducted rocket.
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- Combustion, Explosion, & Shock Waves, 2017, v. 53, n. 3, p. 293, doi. 10.1134/S0010508217030066
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Ignition of a metallized composite solid propellant by a group of hot particles.
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- Combustion, Explosion, & Shock Waves, 2016, v. 52, n. 6, p. 694, doi. 10.1134/S0010508216060095
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Generation of hydrodynamic instability in the gasification region of propellant.
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- Combustion, Explosion, & Shock Waves, 2016, v. 52, n. 6, p. 683, doi. 10.1134/S0010508216060083
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Correlation of parameters in the burning rate law and its influence on intraballistic characteristics of a rocket motor.
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- Combustion, Explosion, & Shock Waves, 2016, v. 52, n. 4, p. 427, doi. 10.1134/S0010508216040067
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Negative erosion effect and the emergence of unstable combustion. 1. Analysis of the models.
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- Combustion, Explosion, & Shock Waves, 2016, v. 52, n. 1, p. 67, doi. 10.1134/S0010508216010093
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Calculation of the characteristics of agglomerates during combustion of high-energy composite solid propellants.
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- Combustion, Explosion, & Shock Waves, 2015, v. 51, n. 5, p. 549, doi. 10.1134/S0010508215050056
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Stability of composite solid propellant ignition by a local source of limited energy capacity.
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- Combustion, Explosion, & Shock Waves, 2014, v. 50, n. 6, p. 670, doi. 10.1134/S0010508214060082
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Calculation of the unsteady internal ballistic parameters of the transition of a solid rocket motor to steady-state operation using the method of characteristics.
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- Combustion, Explosion, & Shock Waves, 2014, v. 50, n. 6, p. 676, doi. 10.1134/S0010508214060094
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On the use of energetic compounds containing small molecules occluded in the structural cavities of the crystal.
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- Combustion, Explosion, & Shock Waves, 2014, v. 50, n. 5, p. 538, doi. 10.1134/S0010508214050086
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