International Journal of Energetic Materials and Chemical Propulsion
Published 6 issues per year
ISSN Print: 2150-766X
ISSN Online: 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
Volume 4, 1997 Issue 1-6
Challenges in Propellants and Combustion − 100 Years after Nobel: The Forth International Symposium on Special Topics in Chemical Propulsion
Stockholm, Sweden, 27−31 May, 1996
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6
Historical Lecture on Alfred B. Nobel
ALFRED NOBEL: FROM GUNPOWDER TO BALLISTIT
ALFRED NOBEL: FROM GUNPOWDER TO BALLISTIT
pp. xvii-xxiii
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.20
Area 1: Chemical Kinetics of Propellant Combustion
ADVANCES IN COMBUSTION-LIKE KINETICS AND MECHANISMS OF POLYMERIC BINDERS
pp. 3-23
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.40
UNUSUAL COMBUSTION BEHAVIOR OF NITRAMINES AND AZIDES
pp. 24-37
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.50
STUDY OF FLAME STRUCTURE, KINETICS AND MECHANISM OF THE THERMAL DECOMPOSITION OF SOLID PROPELLANTS BY PROBING MASS SPECTROMETRY
pp. 38-47
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.60
THEORETICAL STUDY OF HONO REACTIONS WITH H, OH, NO AND NH2 RADICALS
pp. 48-57
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.70
Gas-Phase Reaction Mechanisms for Nitramine Combustion: On the Development of a Comprehensive Reaction Mechanism for Hydrogen/Nitrous Oxide Kinetics
pp. 58-69
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.80
MECHANISTIC STUDIES OF LOW-PRESSURE FLAMES SUPPORTED BY NITROGEN OXIDES
pp. 70-80
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.90
Area 2: Environmental Considerations in Combustion of Solid and Liquid Propellants
TOWARDS THE DEVELOPMENT OF "CLEAN BURNING", LOW FLAME TEMPERATURE SOLID GUN PROPELLANTS
pp. 83-91
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.110
EFFECTS OF ROCKET EXHAUST ON THE LAUNCH SITE ENVIRONMENT AND STRATOSPHERIC OZONE
pp. 92-105
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.120
ENVIRONMENTAL IMPACT ASSESSMENT OF SOLID ROCKET MOTORS GROUND TESTS
pp. 106-117
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.130
ON THERMOCHEMICAL CHARACTERISTICS OF AP/NSAN/HTPB COMPOSITE PROPELLANTS
pp. 118-128
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.140
REALISATION OF AN ECO-FRIENDLY SOLID PROPELLANT BASED ON HTPB -HMX-AP SYSTEM FOR LAUNCH VEHICLE APPLICATIONS
pp. 129-134
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.150
SOIL CONTAMINATED WITH EXPLOSIVES: A SEARCH FOR REMEDIATION TECHNOLOGIES
pp. 135-144
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.160
SOLID PROPELLANT UTILIZATION BY THE BURNING PROPELLANT-COAL AND PROPELLANT-PEAT MIXTURES
pp. 145-152
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.170
Area 3: Recycling of Energetic Materials
BOILER FUEL AS A RECYCLING OPTION FOR ENERGETIC MATERIALS
pp. 167-176
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.200
RECYCLING OF EXCESS AND DEMILITARIZED ENERGETIC MATERIALS IN COMMERCIAL EXPLOSIVE APPLICATIONS
pp. 177-188
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.210
RECENT STUDIES ON THE CHEMICAL CONVERSION OF ENERGETIC MATERIALS TO HIGHER VALUE PRODUCTS
pp. 189-198
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.220
RECYCLING PROPELLANTS AND EXPLOSIVES INTO THE COMMERCIAL EXPLOSIVE INDUSTRY
pp. 199-204
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.230
PROCESSING OF TRINITROTOLUENE-WATER EMULSIONS FOR RECYCLING
pp. 205-212
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.240
PILOT-SCALE BASE HYDROLYSIS PROCESSING OF HMX-BASED PLASTIC-BONDED EXPLOSIVES
pp. 213-220
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.250
CRYOGENIC WASHOUT OF SOLID ROCKET PROPELLANTS
pp. 221-230
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.260
Area 4: New Techniques and Improved Safety in Combustion of Energetic Materials
THE HAZARDS OF SOLID PROPELLANT COMBUSTION
pp. 233-267
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.280
ATOMIC FORCE MICROSCOPY OF HOT SPOTS IN RDX AND AP CRYSTALS
pp. 268-277
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.290
The Importance of Mononitroso Analogues of Cyclic Nitramines to the Assessment of the Safety of HMX-Based Propellants and Explosives
pp. 278-289
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.300
IGNITION OF LIQUID AND SOLID NITROCOMPOUNDS AT FAST COMPRESSION OF GAS INTRUSIONS
pp. 290-301
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.310
EFFECT OF FE2O3 ON THE MATERIAL PROPERTIES OF AP/AL/HTPB BASED PROPELLANTS
pp. 302-312
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.320
THERMOMECHANICAL ASPECTS OF ENERGETIC CRYSTAL COMBUSTION
pp. 313-336
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.330
INSENSITIVE MUNITIONS PROPULSION PROGRESS
pp. 337-344
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.340
COMBUSTION ROLES IN SAFETY OF LESS EXPLOSIVELY SENSITIVE CLASS 1.3 PROPELLANTS
pp. 345-355
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.350
PROPENSITY OF FLAME SPREADING INTO PROPELLANT SLITS UNDER SIMULATED ROCKET-MOTOR ENVIRONMENTS
pp. 356-367
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.360
EVALUATION OF THE EFFECTIVENESS OF AN INDUSTRIAL REPAIR PROCEDURE FOR SOLID PROPELLANT GRAINS
pp. 368-386
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.370
SOLID SOLUTION FORMATION BETWEEN RDX AND COMMON SOLID PROPELLANT BINDERS
pp. 387-394
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.380
CHARACTERIZATION OF WAXES FOR DESENSITIZATION OF EXPLOSIVE COMPOSITIONS
pp. 395-409
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.390
Area 5: Commercial Application in the Combustion of Energetic Materials
ADVANCES IN ENERGETIC MATERIALS MANUFACTURING TECHNOLOGIES AT ICI
pp. 413-429
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.410
"CLEAN" PROPELLANTS FOR COMMERCIAL APPLICATIONS
pp. 430-441
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.420
CLEAN LIQUID AND HYBRID GAS GENERATOR SYSTEM FOR INFLATING CAR AIRBAGS
pp. 442-452
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.430
Future Trends in Gas Generator Systems
pp. 453-456
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.440
UTILIZATION OF PROPELLANTS FOR INFLATOR AND BELT RESTRAINT SYSTEMS
pp. 457-464
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.450
EXPERIMENTAL STUDY OF FLAME-SPREADING PROCESSES OVER Mg/PTFE/Mg THIN FOILS
pp. 465-475
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.460
COMBUSTION AND DETONATION IN PULSED POWER GENERATORS
pp. 476-485
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.470
TWO-PHASE FLAMES A POTENTIAL METHOD FOR MANUFACTURING SUBMICRON METAL OXIDE POWDERS
pp. 486-489
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.480
Area 6: Ignition and Combustion Performance of Propellants for Rocket Propulsion
A SURVEY OF PRESSURE-DRIVEN BURNING OF ENERGETIC SOLIDS WITH ARRHENIUS SURFACE PYROLYSIS
pp. 493-514
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.500
RECENT DEVELOPMENTS AND CHALLENGES IN THE IGNITION AND COMBUSTION OF SOLID PROPELLANTS
pp. 515-548
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.510
RECENT DEVELOPMENTS IN GUN PROPELLANTS AND GUN PROPULSION RESEARCH AT S.N.P.E.
pp. 549-558
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.520
COMBUSTION BEHAVIOR AND THERMOCHEMICAL PROPERTIES OF JA2 PROPELLANT
pp. 559-573
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.530
BALLISTIC AND MICROSTRUCTURAL PROPERTIES OF A HIGHLY FILLED GUN PROPELLANT WITH VARYING THICKNESSES OF INERT SURFACE COATING
pp. 574-586
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.540
IMPROVEMENT OF BALLISTIC CHARACTERISTICS OF GUN PROPELLANTS AND CHARGES USING METALLIC ADDITIVES
pp. 587-593
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.550
BURN RATE STUDEES OF GAS GENERATOR PROPELLANTS CONTAINING AP/RDX
pp. 594-606
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.560
MASS BALANCE IN DETERRENT COATING OF SMOKELESS POWDERS
pp. 607-615
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.570
ADN: A new high performance oxidizer for solid propellants
pp. 616-626
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.580
'ACTIVATED' ALUMINUM AS A STORED ENERGY SOURCE FOR PROPELLANTS
pp. 636-645
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.600
HIGH BURNING RATE SOLID ROCKET PROPELLANTS
pp. 646-660
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.610
EXPERIMENTAL ANALYSIS OF A MINIMUM SMOKE PROPELLANT IGNITION CHARACTERIZATION
pp. 661-667
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.620
A Solid-Phase Model for Plasma Ignition of Solid Propellant
pp. 668-678
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.630
New Insights into the Combustion of AP/HTPB Rocket Propellents: The Catalyst Active Sites and a Combustion Flame Model for The Ferrocene-Catalysed Combustion
pp. 679-692
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.640
EXPERIMENTAL STUDIES OF ALUMINUM AGGLOMERATION IN SOLID ROCKET MOTORS
pp. 693-705
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.650
POLYNIMMO, A CANDIDATE BINDER FOR SOLID FUEL GAS GENERATOR PROPELLANTS
pp. 706-718
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.660
INSTANTANEOUS REGRESSION BEHAVIOR OF HTPB SOLID FUELS BURNING WITH GOX IN A SIMULATED HYBRID ROCKET MOTOR
pp. 719-733
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.670
REAL GAS EFFECTS SIMULATION IN A MODEL GH2/O2 ROCKET THRUST CHAMBER
pp. 734-742
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.680
EFFECTS OF FLAME BEHAVIOR ON A GASEOUS METHANE/OXYGEN SMALL THRUSTER PERFORMANCE
pp. 743-752
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.690
COMBUSTION CHARACTERISTICS IN A GASEOUS HYDROGEN/OXYGEN SMALL THRUSTER
pp. 753-761
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.700
THE EFFECT OF CHEMICALLY INDUCED STRESSES AND DEFORMATIONS ON THE IGNITION OF SOLID PROPELLANTS
pp. 762-773
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.710
MATHEMATICAL MODELING OF OPERATION OF AN ACOUSTIC DAMPER WITH GAS IN ITS INTERNAL CAVITY
pp. 774-782
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.720
IGNITION OF PROPELLANTS: SHAPING AND DEVELOPMENT OF BURNING WAVE AND ITS CHARACTERISTICS
pp. 783-792
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.730
ON CHEMICAL KINETICS OF THE IGNITION OF AP / NSAN / INERT BINDER COMPOSITE PROPELLANTS
pp. 793-803
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.740
Area 7: Combustion Diagnostics
PROPELLANT COMBUSTION DIAGNOSTICS VIA MULTICHANNEL ABSORPTION SPECTROSCOPY
pp. 807-824
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.760
OPTICAL DIAGNOSTICS OF ATOMIZATION AND COMBUSTION FOR CRYOGENIC LIQUID ROCKET PROPULSION
pp. 825-836
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.770
DIAGNOSTICS OF NON-REACTING AND REACTING SUPERSONIC FLOWS IN A SCRAMJET MODEL COMBUSTOR USING NON-INTRUSIVE SPECTROSCOPIC METHODS
pp. 837-848
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.780
GAS TEMPERATURE MEASUREMENTS IN A FLAT FLAME BY TUNABLE DIODE LASER SPECTROSCOPY
pp. 849-862
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.790
THE RESPONSE OF A PYROTECHNIC POWDER UNDER DYNAMIC LOADING CONDITIONS
pp. 863-875
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.800
OVERTONE ABSORPTION SPECTROSCOPY OF SOLID PROPELLANT FLAMES: CO AND N2O CONCENTRATIONS
pp. 876-884
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.810
DETERMINATION OF TEMPERATURE AND OH CONCENTRATION PROFILES OF RDX/CAB PSEUDO PROPELLANTS USING UV/VISIBLE ABSORPTION SPECTROSCOPY
pp. 885-895
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.820
COMBUSTION PHENOMENA OF BORON CONTAINING PROPELLANTS
pp. 896-905
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.830
CHARACTERIZATION OF CONDENSED-PHASE CHEMICAL REACTIONS OF RDX AND NITRAMINE-BASED PROPELLANTS
pp. 906-917
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.840
X-RAY DIAGNOSTICS FOR LOCAL BURNING RATE MEASUREMENT OF SOLID PROPELLANTS
pp. 918-926
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.850
SPECTROSCOPIC INVESTIGATION OF SOLID ROCKET SIGNATURES
pp. 927-933
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.860
CARS MEASUREMENTS OF TEMPERATURE FLUCTUATIONS IN A HIGH PRESSURE GAS TURBINE COMBUSTOR
pp. 934-942
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.870
DIAGNOSTICS AND ACTIVE CONTROL OF ACOUSTIC INSTABILITIES IN COMBUSTORS BY ELECTRICAL DISCHARGES AND PLASMA JETS
pp. 943-761
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.880
COMPOSITE PROPELLANT EXTINCTION BY LASER ENERGY PULSE
pp. 962-971
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.890
IN-CYLINDER MEASUREMENTS OF NO IN A RUNNING DIESEL ENGINE BY MEANS OF LIF DIAGNOSTICS
pp. 972-982
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.900
Area 8: Theoretical Modeling and Numerical Simulation of Combustion Processes of Energetic Materials
NUMERICAL SIMULATION OF DETONATIONS: FUNDAMENTALS AND APPLICATION
pp. 985-997
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.920
SOME DYNAMICS OF ACOUSTIC OSCILLATIONS WITH NONLINEAR COMBUSTION AND NOISE
pp. 998-1013
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.930
MODELING OF TRANSIENT COMBUSTION REGIMES OF ENERGETIC MATERIALS WITH SURFACE EVAPORATION
pp. 1014-1025
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.940
ANOMALOUS GROUP COMBUSTION THEORY: TRANSIENT DUALITY IN GROUP COMBUSTION
pp. 1026-1034
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.950
A PHENOMENOLOGICAL THEORY OF PROPELLANTS' IGNITION AND SUBSEQUENT UNSTEADY COMBUSTION IN HIGH PRESSURE CHAMBERS
pp. 1035-1045
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.960
Ignition and Unsteady Combustion of AP-based Composite Propellants in Subscale Solid Rocket Motors
pp. 1046-1061
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.970
EVALUATION OF THERMOCHEMICAL EROSION OF THE SOLID PROPELLANT ROCKET GRAPHITE NOZZLE THROATS BY INTEGRAL BOUNDARY LAYER TECHNIQUE
pp. 1062-1071
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.980
A NUMERICAL STUDY ON UNSTEADY PRESSURE FLUCTUATIONS OF DAVIS GUN
pp. 1072-1081
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.990
UNSTEADY COMBUSTION OF HOMOGENEOUS ENERGETIC SOLIDS
pp. 1082-1092
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.1000
IMPROVEMENTS TO MODELING OF HOT FRAGMENT CONDUCTIVE IGNITION OF NITRAMINE-BASED PROPELLANTS
pp. 1093-1103
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.1010
AN EIGENVALUE METHOD FOR COMPUTING THE BURNING RATES OF RDX AND HMX MONOPROPELLANTS
pp. 1104-1115
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.1020
A COMPARISON OF SOLID MONOPROPELLANT COMBUSTION AND MODELING
pp. 1116-1132
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.1030
MODELING AND NUMERICAL SIMULATION OF PHYSICOCHEMICAL PROCESSES OCCURRING IN THE TWO-PHASE FOAM LAYER OF BURNING RDX
pp. 1133-1145
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.1040
NONLINEAR TRANSIENT BURNING OF COMPOSITE PROPELLANTS: THE EFFECT OF SOLID PHASE REACTIONS
pp. 1146-1156
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.1050
THE MODEL OF POROUS CARBONIZED PARTICLE COMBUSTION
pp. 1157-1163
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.1060
NUMERICAL SIMULATION OF THE NONSTATIONARY SPATIAL GASDYNAMICS PROCESSES ACCOMPANYING THE PELLETIZED SOLID PROPELLANT COMBUSTION IN A GAS GENERATOR
pp. 1164-1178
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.1070
Latest Issue
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Effects of Fluorinated and Non-Fluorinated Additives on Burning Rates of Boron-Teflon Blends for Solid Rocket Propulsion
Short Overview and Highlights of the History of the German Gel Propulsion Research and Technology Development Activities
Experimental study of boron carbide formation in combustion of boron-containing solid propellants
Electrochemical Burn Rate Acceleration
COMBUSTION OF ALUMINUM PARTICLES IN A STREAM OF STEAM