国际能源材料和化学驱动期刊
每年出版 6 期
ISSN 打印: 2150-766X
ISSN 在线: 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
卷 17, 2018 册 4
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v17.i4
EXPERIMENTAL STUDY OF A LASER IGNITED THRUSTER WITH A POROUS INJECTOR HEAD
pp. 263-286
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2019027382
APPROPRIATENESS OF BURNING RATE MEASURING TECHNIQUE WITH THE MEASURING CONDITIONS AND REQUESTED DATA
pp. 287-302
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2019029021
THERMOCHEMICAL PROPERTIES AND LASER-IGNITION PERFORMANCE OF Al/CuMoO4, Al/CuO/MoO3, Al/CuO AND Al/MoO3 NANOTHERMITES
pp. 303-319
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2019027842
CATALYTIC EFFECTIVITY OF PRINTED MONOLITHIC STRUCTURES WITH HYDROGEN PEROXIDE – MODELING AND EXPERIMENTAL RESULTS
pp. 321-336
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2019028072
OPTICAL CHARACTERIZATION OF THE LASER-INDUCED IGNITION SPARK IN A CRYOGENIC ROCKET COMBUSTOR
pp. 337-347
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2019027786
NEW GREEN AND THERMALLY STABLE SOLID PROPELLANT FORMULATIONS BASED ON TNEF
pp. 349-357
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2019027093
最新一期
将发表的论文
Effect of HMX Content on Thermal Safety Characteristics of Modified Double Base Propellants
40 Years with Chemical Propulsion – Research, Development and Application
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