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verified SJR 0,846 · Q1 • database Scopus / SJR & Web of Science indexed
Journal of Propulsion and Power
United States · American Institute of Aerona...
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Journal of Propulsion and Power

Journal of Propulsion and Power is a journal indexed in SJR in Space and Planetary Science and Fuel Technology with an H index of 121. It has a price of 2100 €. It has an SJR impact factor of 0,846 and it has a best quartile of Q1. It is published in English. It has an SJR impact factor of 0,846.

ISSN: 0748-4658
Publisher: American Institute of Aeronautics and Astronautics Inc. (AIAA)
Category: Space and Planetary Science
Indexation: verifiedScopus / SJR verifiedWeb of Science
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schedule CountryOfPapers database fields
SJR Impact Factor trending_up
0,846 Q1
H-index 121
Acceptance rate pie_chart
24% Selective
Source Acceptance_Rate
Time to publication hourglass_top
NPD
Field NPD
Publication cost (APC) payments
2.100 € Subscription
Non-OA path 0 €

Metrics

Scimago and CountryOfPapers database fields

Scopus / SJR Web of Science

SJR Impact

0,846

H-index

121

Docs (year)

74

Docs 3y

272

Total refs

2920

Cites 3y

764

Citable 3y

257

Cites/Doc 2y

2.87

Ref/Doc

39.46

Immediate OA

2100 €

Embargoed OA

NPD

Non OA / Submission

0 €

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Best articles by citations

Characterization of Flashing Phenomena with Cryogenic Fluid Under Vacuum Conditions

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Wall Temperature Effects on Heat Transfer Coefficient for High-Pressure Turbines

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Development of a Laboratory-Scale System for Hybrid Rocket Motor Testing

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Demonstration of Thrust Vector Control by Hydrogen Peroxide Injection in Hybrid Rockets

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Demonstration of mode transition in a scramjet combustor

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Decomposition of Aluminum Hydride Under Solid Rocket Motor Conditions

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Conjugate Design/Analysis Procedure for Film-Cooled Turbine Airfoil Sections

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Condensed Combustion Products at the Burning Surface of Aluminized Solid Propellant

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Computational Study of Rotating-Stall Inception in Axial Compressors

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Compressible Modeling of the Internal Two-Phase Flow in a Gas-Centered Swirl Coaxial Fuel Injector

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Combustion of Magnesium with Carbon Dioxide and Carbon Monoxide at Low Gravity

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Combustion Characteristics of Aluminum Hydride at Elevated Pressure and Temperature

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Chemical Erosion of Carbon-Carbon/Graphite Nozzles in Solid-Propellant Rocket Motors

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Acoustic boundary layers in solid propellant rocket motors using Navier-Stokes equations

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Carbon-Carbon Nozzle Erosion and Shape-Change Effects in Full-Scale Solid-Rocket Motors

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Burn time measurements of single aluminum particles in steam and CO2 mixtures

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Axial Turbine Blade Tips: Function, Design, and Durability

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Announcements and Acknowledgments

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Analysis of Supersonic Micronozzle Flows

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Analysis of Multivane Radiometer Arrays in High-Altitude Propulsion

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Airblast atomization at conditions of low air velocity

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Aerodynamic Characterization of Linear Aerospike Nozzles in Off-Design Flight Conditions

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Advanced Mixing Control in Supersonic Airstream with a Wall-Mounted Cavity

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Acoustically Consistent Investigation of Combustion Instabilities in a Dump Combustor

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