Works matching DE "SOLID propellant rockets"
Results: 71
GRAVITY MEASUREMENT METHOD OF SOLID ROCKET DRIVE BASED ON SWITCHED RELUCTANCE MOTOR SYSTEM.
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- Thermal Science, 2021, v. 25, n. 6A, p. 4011, doi. 10.2298/TSCI2106011J
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EXPERIMENTAL STUDY ON COMPOSITE SOLID PROPELLANT MATERIAL BURNING RATE USING MATLAB ALGORITHM.
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- Thermal Science, 2016, v. 20, p. S1119, doi. 10.2298/TSCI16S4119T
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Iran's Ballistic Missiles.
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- Strategic Assessment: A Multidisciplinary Journal on National Security, 2009, v. 12, n. 2, p. 29
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The SCOUT-O3 Darwin Aircraft Campaign: rationale and meteorology.
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- Atmospheric Chemistry & Physics Discussions, 2008, v. 8, n. 5, p. 17131, doi. 10.5194/acpd-8-17131-2008
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Testing and Modeling Fuel Regression Rate in a Miniature Hybrid Burner.
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- International Journal of Aerospace Engineering, 2012, p. 1, doi. 10.1155/2012/673838
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Transient Burning Rate Model for Solid Rocket Motor Internal Ballistic Simulations.
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- International Journal of Aerospace Engineering, 2008, p. 1, doi. 10.1155/2008/826070
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A decision approach for multi-stage combined design of solid rocket.
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- Enterprise Information Systems, 2021, v. 15, n. 8, p. 1179, doi. 10.1080/17517575.2020.1739341
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Solid propellant combustion in a high-velocity cross-flow of gases (review).
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- Combustion, Explosion, & Shock Waves, 2016, v. 52, n. 5, p. 497, doi. 10.1134/S0010508216050014
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Mechanism of the negative erosion effect.
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- Combustion, Explosion, & Shock Waves, 2013, v. 49, n. 3, p. 273, doi. 10.1134/S0010508213030039
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Method of the model equation in the theory of unsteady combustion of a solid propellant.
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- Combustion, Explosion, & Shock Waves, 2012, v. 48, n. 1, p. 64, doi. 10.1134/S0010508212010091
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Coagulation of a liquid condensate of aluminum oxide in the combustion chamber of a solid rocket motor.
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- Combustion, Explosion, & Shock Waves, 2011, v. 47, n. 1, p. 55, doi. 10.1134/S0010508211010072
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Analysis of the possibility of steady-state operation of a small-size solid-propellant thruster.
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- Combustion, Explosion, & Shock Waves, 2009, v. 45, n. 5, p. 579, doi. 10.1007/s10573-009-0069-6
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Chemical processes in the HNF flame.
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- Combustion, Explosion, & Shock Waves, 2006, v. 42, n. 5, p. 509, doi. 10.1007/s10573-006-0083-x
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- Article
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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The Use of Monte Carlo Simulation Methods to Calculate the Radiation of Jets of Combustion Products in View of Rotational Spectral Structure.
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- High Temperature, 2003, v. 41, n. 5, p. 694, doi. 10.1023/A:1026157031016
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Improving the completeness of combustion of boron particles in a solid-fuel ducted rocket owing to distributed air supply to the secondary combustor.
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- Doklady Physical Chemistry, 2016, v. 471, n. 2, p. 203, doi. 10.1134/S0012501616120034
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Flight Overloading Effect on the Working-Process Instability in the Combustion Chamber of a Solid-Fuel Rocket Engine.
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- Doklady Physics, 2004, v. 49, n. 9, p. 527, doi. 10.1134/1.1810579
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COMPARATIVE STUDY OF AN ADDITIONAL OXIDIZER CHARGE EFFECT ON SELECTED OPERATIONAL CHARACTERISTICS OF A SOLID-FUEL ROCKET ENGINE.
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- Technical Transactions / Czasopismo Techniczne, 2016, v. 4-M, p. 65, doi. 10.4467/2353737XCT.16.234.5983
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Investigation of high rate mechanical flow followed by ignition for high-energy propellant under dynamic extrusion loading.
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- Defence Technology, 2024, v. 32, p. 336, doi. 10.1016/j.dt.2023.05.009
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Damage-ignition mechanism studies on modified propellant with different crosslinking density under dynamic loading.
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- Defence Technology, 2023, v. 28, p. 155, doi. 10.1016/j.dt.2022.08.006
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Extended Application and Experimental Verification of a New Erosive Burning Model Coupled Heat Transfer between Gas and Grain Based on a Star-Grain Solid Rocket Motor.
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- Energies (19961073), 2022, v. 15, n. 4, p. 1564, doi. 10.3390/en15041564
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Solid Rocket Grain Geometry Modifications for Axial Combustion Instability Symptom Suppression.
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- International Review of Aerospace Engineering, 2010, v. 3, n. 2, p. 102
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Burn-back Equations for High Volumetric Loading Single-grain Dual-thrust Rocket Propellant Configuration.
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- Defence Science Journal, 2011, v. 61, n. 2, p. 165, doi. 10.14429/dsj.61.41
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Successful plant scale production of solid propellant recycling from obsolete ammunition.
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- Journal of Material Cycles & Waste Management, 2017, v. 19, n. 2, p. 898, doi. 10.1007/s10163-016-0495-y
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Design and Performance of Modular 3-D Printed Solid-Propellant Rocket Airframes.
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- Aerospace (MDPI Publishing), 2017, v. 4, n. 2, p. 17, doi. 10.3390/aerospace4020017
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Soviet response to cruise and Pershing.
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- Bulletin of the Atomic Scientists, 1984, v. 40, n. 3, p. 3, doi. 10.1080/00963402.1984.11459184
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SOLID ROCKET MOTOR STAR GRAIN GEOMETRICAL ANALYSIS AND PERFORMANCE MODEL.
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- Annals of the Faculty of Engineering Hunedoara - International Journal of Engineering, 2020, n. 4, p. 193
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Swirl Characteristics of Vortex Valve Variable-Thrust Solid Rocket Motor.
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- Journal of Applied Fluid Mechanics, 2018, v. 11, n. 1, p. 205, doi. 10.29252/jafm.11.01.27658
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Flow modeling in a porous cylinder with regressing walls using semi analytical approach.
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- International Journal of Multiphysics, 2015, v. 9, n. 1, p. 75, doi. 10.1260/1750-9548.9.1.75
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Failure Mode Avoidance of Solid Rocket Motor Pressure Monitoring Joint Seals.
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- Journal of Failure Analysis & Prevention, 2017, v. 17, n. 6, p. 1191, doi. 10.1007/s11668-017-0356-6
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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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Design of the testing system for solid propellant rocket motor thrust measurements using mathematical modelling techniques.
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- Journal of Measurements in Engineering, 2015, v. 3, n. 4, p. 123
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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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On the swirling Trkalian mean flow field in solid rocket motors.
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- Journal of Fluid Mechanics, 2017, v. 824, p. 265, doi. 10.1017/jfm.2017.342
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Design and Analysis of Solid Rocket Composite Motor Case Connector Using Finite Element Method.
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- Polymers (20734360), 2022, v. 14, n. 13, p. 2596, doi. 10.3390/polym14132596
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On the Ratio of Fréchet Random Variables.
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- Quality & Quantity, 2006, v. 40, n. 5, p. 861, doi. 10.1007/s11135-005-5484-5
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一种改进型远程火箭弹发动机点火装置.
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- Ordnance Industry Automation, 2022, v. 41, n. 9, p. 83, doi. 10.7690/bgzdh.2022.09.018
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Coupled Thermo-Structural Analysis Model of Solid Rocket Motor Nozzle considering the Variation of Friction Coefficient under Operating Conditions.
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- International Journal of Aerospace Engineering, 2022, p. 1, doi. 10.1155/2022/4608619
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Coupling of Level Set and Volume of Fluid Methods for Simulations of Transient Internal Flow Field in Solid Rocket Motors.
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- International Journal of Aerospace Engineering, 2021, p. 1, doi. 10.1155/2021/2984992
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Instantaneous Impact Point Guidance with Coast Arcs for Solid Rockets.
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- International Journal of Aerospace Engineering, 2021, p. 1, doi. 10.1155/2021/5571877
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Electrospray Deposition of Energetic Polymer Nanocomposites with High Mass Particle Loadings: A Prelude to 3D Printing of Rocket Motors.
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- Advanced Engineering Materials, 2015, v. 17, n. 1, p. 95, doi. 10.1002/adem.201400151
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Analysis of efficiency of using hybrid propulsion for accelerating small-size rockets starting from the earth surface.
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- Journal of Applied Mechanics & Technical Physics, 2010, v. 51, n. 6, p. 792, doi. 10.1007/s10808-010-0099-6
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- Article
MISIONES DE COHETERÍA EXPERIMENTAL CON PROPELENTE SÓLIDO: MISIÓN SÉNECA, COHETE AINKAA 1.
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- Ciencia e Ingenieria Neogranadina, 2010, v. 20, n. 2, p. 53
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Review of ultrasonic testing technology for bonding interfaces of solid rocket motors.
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- Insight: Non-Destructive Testing & Condition Monitoring, 2021, v. 63, n. 11, p. 648, doi. 10.1784/insi.2021.63.11.648
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Mathematical modelling of the X-ray image of solid rocket motor for quantitative analysis.
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- Insight: Non-Destructive Testing & Condition Monitoring, 2006, v. 48, n. 1, p. 21, doi. 10.1784/insi.2006.48.1.21
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SEM, WAXD AND ED(P)XRFS INVESTIGATIONS ON NEW SORTS OF COKE.
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- Metalurgia, 2009, v. 61, n. 5, p. 45
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Investigation of the Ablative Properties of an EPDM\Kevlar Insulator in a Solid Rocket Motor.
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- Propellants, Explosives, Pyrotechnics, 2022, v. 47, n. 1, p. 1, doi. 10.1002/prep.202100051
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- Article
Thermal Safety of a Gun‐Launched Missile's Solid Rocket Motor Under Conditions of High Environm. Temp. and Overloaded Forces.
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- Propellants, Explosives, Pyrotechnics, 2018, v. 43, n. 12, p. 1277, doi. 10.1002/prep.201800050
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Thermokinetic Analysis and Performance Evaluation of Guanidinium Azotetrazolate Based Gas Generating Composition for Testing of Solid Rocket Motor Nozzle Closures.
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- Propellants, Explosives, Pyrotechnics, 2018, v. 43, n. 10, p. 1006, doi. 10.1002/prep.201800103
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Comparative Study on Infrared Irradiance Emitted from Standard and Real Rocket Motor Plumes.
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- Propellants, Explosives, Pyrotechnics, 2015, v. 40, n. 5, p. 779, doi. 10.1002/prep.201400213
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