Journal of Propulsion and Power

Papers
(The TQCC of Journal of Propulsion and Power is 3. The table below lists those papers that are above that threshold based on CrossRef citation counts [max. 250 papers]. The publications cover those that have been published in the past four years, i.e., from 2021-04-01 to 2025-04-01.)
ArticleCitations
Crossflow Decane Combustion Using Catalytically Decomposed High-Test Peroxide17
Phenomenological Aerodynamic Analysis of an Ejector Exposed to Large Inlet Pulsations12
Chamber Length Limits of a Continuously Variable Geometry Rotating Detonation Combustor11
Shock-Stationary Application of Pseudoshock Models During High-Amplitude Combustion-Driven Unsteadiness9
Thrust Vectoring of Double Divergent Nozzle Using Secondary Fluid Injection9
Improved Hybrid Rocket Performance by Additively Manufactured Gel-Infused Solid Fuels9
Announcements and Acknowledgements8
Computationally Examining the Effect of Plate Thickness on Hole-Emitter-Type Electrospray Thrusters8
Similarity and Scaling in a Liquid-Fuel Ramjet Combustor8
Novel Testing of a Water-Breathing Naval Ramjet at Underwater Cruise Conditions7
Detailed Performance Studies on a Small Electric-Powered Contra-Rotating Ducted Fan Engine7
Numerical Simulations of Fuel Shape Change in Paraffin–Oxygen Hybrid Rocket Engines7
Experimental Characterization of a Hollow Cathode with Iridium–Cerium Alloy7
Combined Heat Shield and Solar Thermal Propulsion System for an Oberth Maneuver7
Effects of Groove Structure on Spray Characteristics of a Throttleable Pintle Injector6
Analysis of Transition to Thermo-Acoustic Instability in Swirl Combustor Using Variational Auto-Encoders6
Multiphase Effects on Solid Rocket Nozzle Performance5
Scramjet Engine Flowpath That Improves Specific Impulse Using JP-7 Fuel5
Transitional Delayed Detached-Eddy Simulation for a Compressor Cascade: A Critical Assessment5
Investigation on Suppression of Hard-Start Phenomena in a Hypergolic Bipropellant Engine5
Increasing Burning Rate and Motor Thrust by Expandable Graphite Additives5
Performance Comparison of Paraffin/Ethanol Fuel Blends in a Laboratory-Scale Hybrid Rocket Motor4
Charactering Catalytic Ignition and Combustion for the Ninety-Percent Hydrogen-Peroxide/Paraffin-Based Hybrid Rocket Engine4
Dynamic Machine Learning Global Optimization Algorithm and Its Application to Aerodynamics4
Three-Dimensional Kinetic Simulations of Carbon Backsputtering in Vacuum Chambers from Ion Thruster Plumes4
Prediction of Burning Characteristics of Dihydroxyglyoxime Composite Propellant4
Improving Base-Drag Corrections for Rotating Detonation Combustor Gross Thrust Measurements4
Regression and Flame Structure in Cavity Flameholding Solid-Fuel Ramjet Fuel Grains4
Fuel Injector Requirements to Achieve Supercritical Flow at the Exit4
Effect of Co- and Counterswirl Air on Swirl Airblast Atomization4
Fundamental Experiment and Numerical Simulation of Ne/Xe Plasma Magnetohydrodynamic Electrical Power Generation4
Transient, Multiscale, Heterogeneous Model of Hydrogen Peroxide Decomposition for 3D-Printed Catalysts4
Observation of Plasma Turbulence in a Hall Thruster Using Microwave Interferometry4
Fuel Temperature Effects on Combustion Stability of a High-Pressure Liquid-Fueled Swirl Flame3
Development of a Liquid-Propellant Rocket Powered by a Rotating Detonation Engine3
Flame Dynamics in an Optically Accessible Solid Fuel Ramjet Combustor3
Computational Analysis and Regression Laws for Nozzle Erosion Prediction in Hybrid Rockets3
Direction Control of Rotating Detonation Waves with Helical Combustion Chambers3
Active Energy Management for Enhanced Engine Transient Operations3
Propellant Surface Evolution of a Coaxial Pulsed Plasma Thruster3
Experimental Investigation on Aluminum-Based Water Ramjet for Propelling High-Speed Underwater Vehicles3
Tandem Energy-Analyzer/Mass-Spectrometer Measurements of an Ionic Liquid Ion Source3
Thermal–Combustion Coupled Instability in Hybrid Rockets with Fuel Blowing3
Numerical Turbulence Modeling in a Transonic Boundary-Layer Ingestion Intake3
Impact of Ammonium Perchlorate Content on Electrically Controlled Gel Polymer Electrolyte Monopropellants3
Hall Thruster System Using Dry Ice Propellant at the Triple Point3
Interaction Behavior of Pulsejet Engines3
Microthrusters’ Combustion Control Using Jellied Propellant Flowing Through an Orifice Plate3
Computational Study of Propulsive Performance of Frozen Nano-Aluminum and Water (ALICE) Mixtures3
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