Works matching DE "ROCKET fuel"
Results: 282
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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Liquid-Phase Reactions in the Catalytic Decomposition of Single-Component Rocket Propellants.
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- Combustion, Explosion, & Shock Waves, 2024, v. 60, n. 4, p. 437, doi. 10.1134/S0010508224040038
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Improvement of the Ignition Performance and Reaction Rate of Boron by Surface Modification.
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- Combustion, Explosion, & Shock Waves, 2024, v. 60, n. 1, p. 110, doi. 10.1134/S0010508224010131
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Thermochemical and Energy Characteristics of Symmetric Nitro and Azido Derivatives of Diazen-Ter-Furazans.
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- Combustion, Explosion, & Shock Waves, 2020, v. 56, n. 3, p. 301, doi. 10.1134/S0010508220030065
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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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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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Reasons for the anomalous dependence of the specific impulse of rocket propellants on the content of borohydride.
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- Combustion, Explosion, & Shock Waves, 2013, v. 49, n. 4, p. 472, doi. 10.1134/S0010508213040102
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Experimental investigation of agglomeration during combustion of aluminized solid propellants in an acceleration field.
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- Combustion, Explosion, & Shock Waves, 2009, v. 45, n. 1, p. 32, doi. 10.1007/s10573-009-0005-9
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Burning of Nano-Aluminized Composite Rocket Propellants.
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- Combustion, Explosion, & Shock Waves, 2005, v. 41, n. 6, p. 680, doi. 10.1007/s10573-005-0080-5
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Statistical simulation of aluminum agglomeration during combustion of heterogeneous condensed mixtures.
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- Combustion, Explosion, & Shock Waves, 2005, v. 41, n. 2, p. 174, doi. 10.1007/s10573-005-0020-4
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Experimental Study of Thrust Performance of a Hybrid Rocket Motor with Various Methods of Oxidizer Injection.
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- Combustion, Explosion, & Shock Waves, 2004, v. 40, n. 4, p. 386, doi. 10.1023/B:CESW.0000033560.34907.5e
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Macrokinetics of Combustion of Monodisperse Agglomerates in the Flame of a Model Solid Propellant.
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- Combustion, Explosion, & Shock Waves, 2003, v. 39, n. 5, p. 552, doi. 10.1023/A:1026113902771
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Microbial‐Mediated Reduction of Perchlorate in Groundwater.
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- Journal of Environmental Quality, 1998, v. 27, n. 4, p. 750, doi. 10.2134/jeq1998.274750x
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Baikonur 2.0: 'inland-offshore' space economies in post-Soviet Kazakhstan.
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- Culture, Theory & Critique, 2021, v. 62, n. 1/2, p. 96, doi. 10.1080/14735784.2021.1929363
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テーパー管への静電容量型ボイド率計の適用に関する研究.
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- Japanese Journal of Multiphase Flow, 2024, v. 38, n. 2, p. 157
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Off-Design Combustion in Liquid-Propellant Rocket Engine with High-Frequency Instability.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2019, v. 62, n. 6, p. 331, doi. 10.2322/tjsass.62.331
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Solid-propellant gas generators with a gas flow rate stabilization system.
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- Doklady Chemistry, 2015, v. 463, n. 1, p. 189, doi. 10.1134/S0012500815070022
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Design Optimization of Propellant Grain and Nozzle Contour to Improve Performance of Solid Rocket Propulsion.
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- Journal of Engineering & Technological Sciences, 2022, v. 54, n. 5, p. 963, doi. 10.5614/j.eng.technol.sci.2022.54.5.8
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Performance Optimization and Toxicity Effects of the Electrochemical Oxidation of Octogen.
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- Catalysts (2073-4344), 2022, v. 12, n. 8, p. 815, doi. 10.3390/catal12080815
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Study of thermal decomposition mechanisms and low-level detection of explosives using pulsed photoacoustic technique.
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- Applied Physics B: Lasers & Optics, 2015, v. 121, n. 2, p. 193, doi. 10.1007/s00340-015-6218-6
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A Global Inventory of Ice‐Related Morphological Features on Dwarf Planet Ceres: Implications for the Evolution and Current State of the Cryosphere.
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- Journal of Geophysical Research. Planets, 2019, v. 124, n. 7, p. 1650, doi. 10.1029/2018JE005699
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ROCKET ENGINES' SOLID PROPELLANTS AND COMBUSTION PRODUCTS.
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- Science & Military Journal, 2024, v. 19, n. 2, p. 36, doi. 10.52651/sam.a.2024.2.36-42
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Influence of Hydrocarbon Rocket Fuel Kerosene T-1 on the Physical and Geochemical Properties of Different Soil Types.
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- Water, Air & Soil Pollution, 2023, v. 234, n. 7, p. 1, doi. 10.1007/s11270-023-06472-9
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Other states of H2.
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- Chemical Engineering, 2021, v. 128, n. 8, p. N.PAG
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The Recycling of Substandard Rocket Fuel N,N-Dimethylhydrazine via the Involvement of Its Hydrazones Derived from Glyoxal, Acrolein, Metacrolein, Crotonaldehyde, and Formaldehyde in Organic Synthesis.
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- International Journal of Molecular Sciences, 2023, v. 24, n. 24, p. 17196, doi. 10.3390/ijms242417196
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Treatment of Substandard Rocket Fuel 1,1-Dimethylhydrazine via Its Methylene Derivative into Heterocycles Based on Pyrrolo-[3,4c]Quinolines, Cyclododeca[b]piran and Pyrrole.
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- International Journal of Molecular Sciences, 2023, v. 24, n. 17, p. 13076, doi. 10.3390/ijms241713076
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Effect of Unsymmetrical Dimethylhydrazine on Isolated Heart and Lymphatic Vessels.
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- Bulletin of Experimental Biology & Medicine, 2022, v. 172, n. 3, p. 297, doi. 10.1007/s10517-022-05380-y
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Kompozit Roket Yakıtının Yanma Hızı Üzerine Ortam Basıncının ve Başlangıç Sıcaklığının Etkileri.
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- International Journal of Engineering Research & Development (IJERAD), 2023, v. 15, n. 2, p. 371, doi. 10.29137/umagd.1213570
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1-Formyl-2,2-dimethylhydrazine as a new decomposition product of 1,1-dimethylhydrazine.
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- International Journal of Environmental Analytical Chemistry, 2007, v. 87, n. 5, p. 351, doi. 10.1080/03067310601068882
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Afterburning effect on thermal environment of four-engine liquid rockets at different altitudes.
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- Engineering Applications of Computational Fluid Mechanics, 2021, v. 15, n. 1, p. 1134, doi. 10.1080/19942060.2021.1947896
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Synthesis of 2-substituted aminothiazol-4(5 H)-ones proceeding from carboxylactones.
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- Russian Journal of Organic Chemistry, 2011, v. 47, n. 8, p. 1204, doi. 10.1134/S1070428011080148
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The Lunar Rush: Mining the Moon.
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- International Policy Digest, 2024, p. 2
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Designing the bioproduction of Martian rocket propellant via a biotechnology-enabled in situ resource utilization strategy.
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- Nature Communications, 2021, v. 12, n. 1, p. 1, doi. 10.1038/s41467-021-26393-7
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Novel Polyurethanes Based on Recycled Polyethylene Terephthalate: Synthesis, Characterization, and Formulation of Binders for Environmentally Responsible Rocket Propellants.
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- Polymers (20734360), 2021, v. 13, n. 21, p. 3828, doi. 10.3390/polym13213828
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Vortices generation in the reactive flow on the evaporative surface.
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- Journal of Mechanical Science & Technology, 2015, v. 29, n. 2, p. 563, doi. 10.1007/s12206-015-0116-z
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Equatorial Perturbation Driven Reaction Bifurcation in Non‐Heme Iron Complexes for Chlorite Oxidation.
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- European Journal of Inorganic Chemistry, 2023, v. 26, n. 33, p. 1, doi. 10.1002/ejic.202300380
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Investigations on Internal Ballistic Characteristics of Pasty Propellant Rocket Engine.
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- International Journal of Aerospace Engineering, 2021, p. 1, doi. 10.1155/2021/9952209
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Quantification of transformation products of rocket fuel unsymmetrical dimethylhydrazine in air using solid‐phase microextraction.
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- Journal of Separation Science, 2022, v. 45, n. 2, p. 614, doi. 10.1002/jssc.202100684
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Reactivity analysis of ammonium dinitramide binary mixtures based on ab initio calculations and thermal analysis.
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- Journal of Thermal Analysis & Calorimetry, 2019, v. 138, n. 4, p. 2615, doi. 10.1007/s10973-019-08557-2
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Thermal study of the decomposition of HTPB hybrid rocket fuel in the presence of azo-tetrazolate-based high nitrogen content high energy materials.
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- Journal of Thermal Analysis & Calorimetry, 2018, v. 134, n. 3, p. 1785, doi. 10.1007/s10973-018-7490-6
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DMA of polyester-based polyurethane elastomers for composite rocket propellants containing different energetic plasticizers.
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- Journal of Thermal Analysis & Calorimetry, 2018, v. 131, n. 1, p. 595, doi. 10.1007/s10973-016-5945-1
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Using thermal methods to understand the interactions between a rocket propellant and igniter material.
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- Journal of Thermal Analysis & Calorimetry, 2018, v. 131, n. 1, p. 379, doi. 10.1007/s10973-017-6830-2
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Thermal decomposition properties and compatibility of CL-20 with binders HTPB, PBAN, GAP and polyNIMMO.
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- Journal of Thermal Analysis & Calorimetry, 2015, v. 119, n. 3, p. 1931, doi. 10.1007/s10973-015-4418-2
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Artificial ageing of double base rocket propellant.
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- Journal of Thermal Analysis & Calorimetry, 2009, v. 96, n. 2, p. 523, doi. 10.1007/s10973-008-9044-9
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Thermal degradation of a composite solid propellant examined by DSC.
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- Journal of Thermal Analysis & Calorimetry, 2004, v. 75, n. 2, p. 551, doi. 10.1023/B:JTAN.0000027145.14854.f0
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Mechanical analysis on rocket propellants.
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- Journal of Thermal Analysis & Calorimetry, 2003, v. 72, n. 3, p. 921, doi. 10.1023/A:1025082602232
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The effect of residual S<sup>2−</sup> and Cl<sup>−</sup> on the corrosion and mechanical property of resistance spot welded joints in rocket storage tank.
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- Journal of Materials Science, 2024, v. 59, n. 35, p. 16707, doi. 10.1007/s10853-024-10141-5
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State-space theory–based closed-loop control of machining error of thin-walled part modeling and application.
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- International Journal of Advanced Manufacturing Technology, 2023, v. 127, n. 3/4, p. 1721, doi. 10.1007/s00170-023-11542-7
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Load Capacity of Concave Conical Shells with Randomly Positioned Circular Cutouts.
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- Experimental Mechanics, 2023, v. 63, n. 7, p. 1223, doi. 10.1007/s11340-023-00986-3
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A Unique Optical System Design and Implementation of X-Ray system to Non-destructive Tests Solid Fuel missiles.
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- Przegląd Elektrotechniczny, 2024, v. 2024, n. 2, p. 1, doi. 10.15199/48.2024.02.01
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