International Journal of Energetic Materials and Chemical Propulsion
年間 6 号発行
ISSN 印刷: 2150-766X
ISSN オンライン: 2150-7678
IF:
0.7
5-Year IF:
0.7
Immediacy Index:
0.1
Eigenfactor:
0.00016
JCI:
0.18
SJR:
0.313
SNIP:
0.6
CiteScore™::
1.6
H-Index:
16
Indexed in
巻 5, 2002 発行 1-6
Combustion of Energetic Materials: The Fifth International Symposium on Special Topics in Chemical Propulsion
Stresa, Italy, 18−22 June, 2000
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6
Area 1: Reaction Kinetics of Energetic Materials (Solid, Liquid, and Gel Propellants)
CHEMICAL AND PHYSICAL PROCESSES THAT CONTROL THE THERMAL DECOMPOSITION OF RDX AND HMX
pp. 3-21
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.30
PYROLYSIS STUDIES OF THE BURNING MECHANISMS OF HIGH-NITROGEN COMPOUNDS
pp. 22-30
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.40
FORMATION AND DECOMPOSITION OF CH2N AND CH2NO IN THE COMBUSTION OF RDX and HMX STUDIED BY QUANTUM CHEMICAL AND STATISTICAL THEORY CALCULATIONS
pp. 31-39
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.50
CONTAINED LOW PRESSURE COMBUSTION OF NIKE AND IMPROVED HAWK ROCKET MOTORS: EXPERIMENTAL TECHNIQUES AND EMISSIONS MEASUREMENTS
pp. 40-49
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.60
Area 2: Recycling of Energetic Materials
RECENT ADVANCES IN THE CHEMICAL CONVERSION OF ENERGETIC MATERIALS
pp. 52-61
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.80
CONVERSION OF DEMILITARIZED TNT TO HIGHER VALUE PRODUCTS
pp. 62-70
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.90
COMBUSTION PROPERTIES RELEVANT TO COFIRING OF SOLID ROCKET MOTOR WASHOUT MATERIAL
pp. 71-80
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.100
AEROSOL EMISSION MEASUREMENTS OF ROCKET MOTORS FROM CONTAINED OPEN BURN EVENTS
pp. 81-87
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.110
Area 3: Combustion Performance of Hybrid and Solid Rocket Motors
HYBRID PROPULSION FOR SMALL SATELLITES DESIGN LOGIC AND TESTS
pp. 90-100
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.130
SURFACE HEAT RELEASE OF HTPB-BASED FUELS IN OXYGEN RICH ENVIRONMENTS
pp. 101-115
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.140
THE ADVANCED TECHNOLOGY OF PREVENTION OF THE ANOMALOUS COMBUSTION REGIMES DEVELOPMENT IN THE SUBMARINE'S BALLISTIC ROCKET WITH LARGE-SIZED SPRM
pp. 116-131
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.150
EXPERIMENTAL AND NUMERICAL STUDY OF CASTING PROCESS EFFECTS ON SMALL SCALE SOLID ROCKET MOTOR BALLISTIC BEHAVIOR
pp. 132-145
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.160
BURNING RATE DATA REDUCTION OF SMALL-SCALE TEST MOTORS
pp. 146-160
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.170
PARAMETRIC INVESTIGATION ON SIMILARITY AND SCALE EFFECTS IN HYBRID MOTORS
pp. 161-169
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.180
Area 4: Ignition and Combustion of Energetic Materials
THE STATUS OF GEL PROPELLANTS IN YEAR 2000
pp. 172-194
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.200
COMBUSTION CHARACTERISTICS OF KEROSENE CONTAINING ALEX® NANO-ALUMINUM
pp. 195-205
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.210
COMBUSTION OF GELLED RP-1 PROPELLANT WITH ALEX® PARTICLES IN GASEOUS OXYGEN ATOMIZED SPRAYS
pp. 206-218
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.220
COMBUSTION PHENOMENA OF A SOLID PROPELLANT BASED ON ALUMINIUM POWDER
pp. 219-225
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.230
COMBUSTION OF SOLID PROPELLANT SANDWICHES: EFFECT OF BINDER OXYGENATION AND FINITE PECLET NUMBER
pp. 226-235
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.240
SICOMIN-ROT K 3130 S AS A BURNING RATE MODIFIER
pp. 236-243
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.250
STUDY ON THE ACTION TEMPERATURE OF CATALYSTS TO SOLID PROPELLANT BURNING RATE USING EMBEDDED THERMOCOUPLE
pp. 244-250
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.260
COMBUSTION PHENOMENA OF THE GUN PROPELLANT JA2
pp. 251-262
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.270
AN/AD/Mg IGNITION BY CO2 LASER RADIATION
pp. 263-273
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.280
ACOUSTIC EMISSION OF UNDERWATER BURNING SOLID ROCKET PROPELLANTS
pp. 274-283
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.290
LASER IGNITION CHARACTERIZATION OF N-5 DOUBLE-BASE SOLID PROPELLANT
pp. 284-295
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.300
The Nimic Energetic Materials Compendium (EMC)
pp. 296-303
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.310
Area 5: Energetic Material Defects and Rocket Engine Flowfields
INVESTIGATION OF COMBUSTING FLOW FIELD IN COMPOSITE PROPELLANT CRACKS
pp. 306-315
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.330
EXPERIMENTAL INVESTIGATION OF EROSIVE BURNING OF COMPOSITE PROPELLANTS UNDER SUPERSONIC CROSSFLOWS
pp. 316-329
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.340
IMPROVEMENT OF FLAMEHOLDING CHARACTERISTICS BY INCIDENT SHOCK WAVES IN SUPERSONIC FLOW
pp. 330-339
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.350
ANALYSIS AND TESTING OF FUEL REGRESSION RATE CONTROL IN SOLID FUEL RAMJETS
pp. 340-353
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.360
INFLUENCE OF MICROCRACKING ON PRESSURE-DEPENDENT ENERGETIC CRYSTAL COMBUSTION
pp. 354-359
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.370
EXPERIMENTAL STUDY OF TYPICAL DEFECT PROPAGATION PROCESSES IN SOLID ROCKET MOTORS
pp. 360-365
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.380
PARAMETRIC INVESTIGATION OF SUPERSONIC COMBUSTION OF SOLID FUELS
pp. 366-374
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.390
Area 6: Metal Combustion
TESTING OF METAL POWDERS BEHAVIOR IN A HOT STAGE MICROSCOPE
pp. 377-383
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.410
FLAME SPREADING AND VIOLENT ENERGY RELEASE PROCESS OF ALUMINUM TUBING IN LIQUID AND GASEOUS OXYGEN ENVIRONMENTS
pp. 384-396
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.420
EVOLUTION OF ALUMINUM AGGLOMERATES MOVING IN COMBUSTION PRODUCTS OF MODEL SOLID PROPELLANT
pp. 397-406
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.430
EXPERIMENTAL OBSERVATIONS ON DISRUPTIVE BURNING OF COATED ALUMINUM PARTICLES
pp. 407-411
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.440
EXPERIMENTAL STUDY OF EVOLUTION OF CONDENSED COMBUSTION PRODUCTS IN GAS PHASE OF BURNING SOLID ROCKET PROPELLANT
pp. 412-426
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.450
INVESTIGATION OF FUEL-RICH BORON COMBUSTION IN A PRESSURIZED COMBUSTION BOMB
pp. 427-437
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.460
COMBUSTION AND FLAME SPREADING OF ALUMINUM TUBING IN HIGH PRESSURE OXYGEN
pp. 438-452
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.470
EFFECTS OF FLUORINE-CONTAINING SPECIES ON THE IGNITION AND COMBUSTION OF BORON PARTICLES: EXPERIMENT AND THEORY
pp. 453-463
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.480
Area 7: Pyrolysis and Combustion Processes of New Ingredients and Applications
ENERGETIC MATERIAL COMBUSTION STUDIES ON PROPELLANT FORMULATIONS AND ITS COMPONENTS
pp. 466-477
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.500
SENSITIVITY PROPERTIES AND BURNING RATE CHARACTERISTICS OF HIGH ENERGY DENSITY MATERIALS AND THE PROPELLANTS CONTAINING THESE MATERIALS
pp. 478-485
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.510
STRUCTURE OF AMMONIUM DINITRAMIDE FLAME AT 4.0 MPa
pp. 486-491
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.520
COMBUSTION PECULIARITIES OF ADN AND ADN-BASED MIXTURES
pp. 502-512
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.540
BURNING RATE AND PRESSURE DEFLAGRATION LIMIT (PDL) CHARACTERISTICS OF A GAP/AP PROPELLANT SYSTEM
pp. 513-522
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.550
DIFFUSION FLAME STRUCTURE OF HNF SANDWICHES
pp. 523-532
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.560
COMBUSTION STUDIES OF NITRAMINE CONTAINING ENERGETIC MATERIALS
pp. 533-545
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.570
REFORMING AND PYROLYSIS OF LIQUID HYDROCARBONS AND PARTIALLY OXIDIZED FUELS FOR HYPERSONIC PROPULSION
pp. 546-562
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.580
BURNING RATE CHARACTERIZATION OF OXSOL LIQUID OXIDIZER
pp. 563-575
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.590
FLAME STRUCTURE OF HYDRAZINIUM NITROFORMATE
pp. 576-586
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.600
HNF/HTPB BASED COMPOSITE PROPELLANTS
pp. 587-596
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.610
Area 8: Theoretical Modeling and Numerical Simulation of Combustion Processes of Energetic Materials
THEORETICAL ANALYSIS OF MODERN ETC-CONCEPTS
pp. 599-605
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.630
MODEL FORMULATION OF LASER INITIATION OF EXPLOSIVES CONTAINED IN A SHELL
pp. 606-621
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.640
FIRST-PRINCIPLES SIMULATION OP GAS-PHASE DDT AND THE EFFECTS OF HOT-SPOT FORMATION
pp. 622-632
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.650
AEROTHERMOCHEMICAL MODEL FOR THE INTERIOR BALLISTICS OF SOLID PROPELLANT ROCKET MOTORS
pp. 633-645
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.660
NUMERICAL ANALYSIS OF GRAIN BURNBACK IN SOLID PROPELLANTS
pp. 646-651
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.670
MASS TRANSFER EFFECTS ON SOUND PROPAGATION IN A DROPLET-GAS MIXTURE
pp. 652-661
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.680
A NUMERICAL SIMULATION OF A PULSE DETONATION ENGINE WITH HYDROGEN FUELS
pp. 662-672
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.690
NUMERICAL SIMULATION OF SOLID MOTOR IGNITION TRANSIENT
pp. 673-688
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.700
ON SINGLE CRYSTAL REACTION INITIATION FOR THERMOMECHANICAL IGNITION MODELS
pp. 689-698
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.710
PREDICTION OF HYBRID FUEL REGRESSION RATE IN CONFINED TURBULENT BOUNDARY LAYER COMBUSTION
pp. 699-711
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.720
Area 9: Combustion Diagnostic Techniques
ELASTIC LASER SCATTERING AS A DIAGNOSTIC TOOL IN REACTING TWO-PHASE SYSTEMS
pp. 714-724
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.740
CRITICAL ASSESSMENT OF THE MICROWAVE METHOD FOR MEASURING STEADY-STATE AND TRANSIENT REGRESSION RATES OF SOLIDS
pp. 725-732
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.750
DETERMINATION OF THE TEMPERATURE OF CONDENSED PARTICLES WITHIN FLAME BY THEIR RADIATION
pp. 733-741
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.760
COMPARISON OF PIV AND COLOUR-SCHLIEREN MEASUREMENTS OF THE COMBUSTION PROCESS OF BORON PARTICLE CONTAINING SOLID FUEL SLABS IN A REARWARD FACING STEP COMBUSTOR
pp. 742-752
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.770
QUICK SPECTROSCOPIC DIAGNOSTICS FOR THE FLAME TEMPERATURE
pp. 753-761
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.780
IMAGING OF MIXING AND COMBUSTION PROCESSES IN A SUPERSONIC COMBUSTION RAMJET CHAMBER
pp. 762-772
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.790
QUANTITATIVE MEASUREMENT OF FLAME GENERATED PARTICULATE OXIDE BY INTERFEROMETRY TECHNIQUE
pp. 773-780
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.800
SPONTANEOUS RADIATION HEAT FEEDBACK MEASUREMENTS IN RADIAL BURNING PROPELLANT SAMPLES
pp. 781-790
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.810
Area 10: Propellant and Rocket Motor Stability
NONLINEAR COMBUSTION IN SOLID PROPELLANT ROCKET MOTORS
pp. 793-802
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.830
EXAMPLES OF UNSTEADY COMBUSTION IN NON-METALLIZED PROPELLANTS
pp. 803-813
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.840
ACTIVE DAMPING OF COMBUSTION INSTABILITIES WITH OSCILLATORY LIQUID FUEL SPRAYS
pp. 814-824
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.850
LIMIT CYCLES FOR SOLID PROPELLANT BURNING RATE AT CONSTANT PRESSURE
pp. 825-836
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.860
CHARACTERISTIC FEATURES OF BURNING-RATE RESPONSE FUNCTIONS: A REVIEW
pp. 837-853
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.870
HMX T-BURNER PRESSURE COUPLED RESPONSE AT 200, 500, AND 1000 PSI
pp. 854-866
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.880
THE STATIONARY MODES OF THE REACTION FRONT AND THEIR STABILITY FOR SOLID MEDIA WITH REGARD TO CHEMICALLY INDUCED INTERNAL STRESSES AND STRAINS
pp. 867-878
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.890
A COMPUTATIONAL STUDY OF THE L* INSTABILITY WITH A NONLINEAR FREQUENCY
pp. 879-888
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.900
FREQUENCY RESPONSE OF A MODEL SUBSCALE ROCKET MOTOR
pp. 889-902
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.910
CHARGE DESIGN AND NON-ACOUSTIC INSTABILITY OF SOLID ROCKET MOTOR
pp. 903-917
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.920
T-BURNER RESPONSE ANALYSIS USING THE SPP/SSP CODE
pp. 918-926
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.930
Area 11: Commercial Applications of Energetic Materials
Explosively Generated Supercritical Water for Deploying Airbags
pp. 929-940
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.950
Prediction of Airbag Inflator Performance
pp. 941-948
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.960
ENERGERIC MATERIALS AS GAS GENERATORS IN EXPLOSIONS SUPPRESSION SYSTEMS
pp. 949-959
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.970
CHARACTERIZATION OF THE COMBUSTION BEHAVIOR OF GAS-GENERATING PYROTECHNICS USING GUN PROPELLANT TECHNOLOGY METHODS
pp. 960-973
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.980
CHARACTERIZATION OF COMBUSTION SPECIES BY REAL TIME FTIR SPECTROSCOPY AT GAS GENERATOR OPERATING PRESSURE
pp. 974-984
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.990
DEVELOPMENT OF PASSIVATED PYROPHORIC METAL POWDERS (HAFNIUM AND ZIRCONIUM) WITH REDUCED ELECTROSTATIC DISCHARGE (ESD) SENSITIVITY
pp. 985-993
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.1000
COMBUSTION SYNTHESIS OF SiO, IN PREMIXED FLAMES
pp. 994-1003
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.1010
Area 12: Thermal Insulation and Ablation Processes
DEGRADATION OF A THERMAL INSULATOR UNDER VIBRATION AND ACCELERATION
pp. 1006-1017
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.1030
THERMAL PROTECTION WALL-EFFECT ON THE COMBUSTION OF A SOLID PROPELLANT AT SUBATMOSPHERIC PRESSURE
pp. 1018-1027
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.1040
THERMAL DECOMPOSITION OF 1,3,3-TRINITROAZETIDINE IN GAS AND LIQUID PHASE
pp. 1028-1030
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.1050
CHEMICAL CONVERSION OF 2.4.6-TRINITROTOLUENE (TNT) TO NEW HIGH PERFORMANCE POLYMERS
pp. 1031-1047
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.1060
BALLISTIC AND COMBUSTION PROPERTIES OF HIGH-PRESSURE EXPONENT HYDROCARBON-BASED FUEL-RICH PROPELLANTS
pp. 1048-1058
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.1070
ZERO-DIMENSIONAL UNSTEADY INTERNAL BALLISTIC MODELING
pp. 1059-1071
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.1080
SHOCK-WAVE CALCULATION MODEL FOR DETONATION OF MULTICOMPONENT ENERGY CARRIER CONTAINING COMBUSTIBLE PHASE
pp. 1072-1089
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.1090
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