International Journal of Energetic Materials and Chemical Propulsion
Выходит 6 номеров в год
ISSN Печать: 2150-766X
ISSN Онлайн: 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
Том 22, 2023 Выпуск 1
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v22.i1
RELATIVE EXPLOSIVE FORCE OF Al/MoO3 NANOCOMPOSITE/POLYMERIC BINDER
pp. 1-10
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2022046800
ACOUSTIC ADMITTANCE OF AN ALUMINIZED COMPOSITE SOLID PROPELLANT BY LASER DOPPLER VELOCIMETRY AT LOW PRESSURE
pp. 11-22
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2022045066
FLIGHT DEMONSTRATION OF A GAP/N2O DIRECT INJECTION GAS-HYBRID ROCKET SYSTEM USING A SMALL ROCKET
pp. 23-34
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2023043424
A STUDY ON THE RECENT ADVANCES IN THE DESIGN OF MEMS-BASED SOLID MICROTHRUSTERS
pp. 35-56
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v22.i1.40
EFFECT OF CATALYZER ON PRIMARY COMBUSTION AND MECHANICAL PROPERTIES OF HIGHLY METALIZED FUEL-RICH PROPELLANTS
pp. 57-75
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2023046659
A NOVEL METHOD TO ANALYZE THE SELF-EXCITED AND PULSED T-BURNER EXPERIMENTAL DATA AT WIDE PRESSURE AND FREQUENCY RANGES
pp. 77-92
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2023046469
Последний выпуск
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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