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 2021-09-01 to 2025-09-01.)
ArticleCitations
Announcements and Acknowledgements20
Experimental Characterization of a Hollow Cathode with Iridium–Cerium Alloy19
Prediction of Burning Characteristics of Dihydroxyglyoxime Composite Propellant15
Detailed Performance Studies on a Small Electric-Powered Contra-Rotating Ducted Fan Engine14
Combined Heat Shield and Solar Thermal Propulsion System for an Oberth Maneuver14
Numerical Simulations of Fuel Shape Change in Paraffin–Oxygen Hybrid Rocket Engines13
Expandable Graphite, a Novel Regression Rate Enhancer in the Solid Fuel Ramjet12
Correlation for Restart Boundaries of Simplified Two-Dimensional Hypersonic Inlets12
Effect of Co- and Counterswirl Air on Swirl Airblast Atomization12
Overview of Selected Serpentine Duct Simulations Using Computational Fluid Dynamics11
Direction Control of Rotating Detonation Waves with Helical Combustion Chambers11
Acoustic Waves Generated in Hypergolic Drop Tests of Low- and High-Volatility Fuels11
Preparation, Ignition, and Combustion of Boron Fuels with CuO as an Additive10
Characterizing Hypergolic Propellants Using Impinging Jets and Droplets in Acoustic Levitation10
Dynamic Regulation Process of the Variable-Geometry Power Turbine10
Stochastic Emission in Passively Fed Single-Emitter Porous-Media Ionic Liquid Ion Sources9
Driving Mechanisms in Low-Order Modeling of Longitudinal Combustion Instability8
Numerical and Experimental Study of an Aircraft Igniter Plasma Jet Discharge8
Multi-Element Gaseous Methane–Oxygen Rocket Combustor Optimization for Modern Space-Flight Technology8
Data-Driven Wall Pressure Reconstruction and Sparse Sensor Optimization for Supersonic Nozzles8
Family of Skeletal Reaction Mechanisms for Methane–Oxygen Combustion in Rocket Propulsion8
Operation and Power Generation of a Disk-Shaped Pressure Gain Combustor7
Machine-Learning-Based Rotating Detonation Engine Diagnostics: Evaluation for Application in Experimental Facilities7
Effects of Thermal/Chemical Nonequilibrium on a High-Mach Ethylene-Fueled Scramjet7
Effect of Varying Secondary Swirl Injector Location on Performance of Hybrid Rocket7
General Burnback Analysis for Anisotropic and Heterogeneous Solid Propellants7
Advancing Mistuning Identification and Dynamic Modeling of Blisks Through Blade Detuning Tests6
Effect of Fuel Injection Strategy on Generic Scramjet Combustor Operation6
Fully Coupled Analysis of Aerothermoelastic Deformation of a Scramjet Inlet6
Loss Mechanisms of Shrouded Stator Cavity Flow in an Axial Compressor6
Surface Structure of Reacting Solid Ramjet Fuels6
Active Flow Control in Compressor Cascades with Steady and Pulsed Jets6
Contribution of Unsteadiness to Solid Fuel Burning Characteristics in a Scramjet Combustor6
Experimental Investigation on Atomization of JP-10 Slurry Jets Containing Boron Nanoparticles5
Fundamental Experiment and Numerical Simulation of Ne/Xe Plasma Magnetohydrodynamic Electrical Power Generation5
Impact of Ammonium Perchlorate Content on Electrically Controlled Gel Polymer Electrolyte Monopropellants5
Experimental Investigation of Throttleable H2O2 and Polypropylene Hybrid Rocket Motor5
Injection Temperature and Scheme Effects on Neutral Flow Dynamics in Hall Thrusters5
Experimental Investigation on Aluminum-Based Water Ramjet for Propelling High-Speed Underwater Vehicles5
Multipoint Aerodynamic Optimization of Three-Dimensional Ultra-High-Bypass-Ratio Engine Intakes5
Performance of Novel Electrode Structures for Electrically Controlled Solid Propellant5
Crossflow Decane Combustion Using Catalytically Decomposed High-Test Peroxide5
Improved Hybrid Rocket Performance by Additively Manufactured Gel-Infused Solid Fuels5
Numerical Modeling to Investigate the Aerodynamics of a Boundary-Layer Ingested Transonic Fan4
Radial Mass Flow Rate Partition on LOx/GCH4 Pintle Injector Configurations4
Delayed Detached-Eddy Simulations of Rough-Wall Turbulent Reactive Flows in a Supersonic Combustor4
Beam Misalignment Effects on Microwave Rocket Propulsion Performance4
Interaction Behavior of Pulsejet Engines4
Thermal–Combustion Coupled Instability in Hybrid Rockets with Fuel Blowing4
Numerical Turbulence Modeling in a Transonic Boundary-Layer Ingestion Intake4
Fuel Regression Characteristics of Axial-Injection End-Burning Hybrid Rockets Using LOX4
Low-Order Autoignition Modeling for Hydrogen Transverse Jets4
Wave Detection and Tracking Within a Rotating Detonation Engine Through Object Detection4
Computational Analysis and Regression Laws for Nozzle Erosion Prediction in Hybrid Rockets4
Impact of Future Low-Emissions Combustor Technology on Acoustic Scaling Laws4
Design and Performance of an Electrowetting Ionic Liquid Electrospray Thruster Prototype4
Computationally Examining the Effect of Plate Thickness on Hole-Emitter-Type Electrospray Thrusters3
Simplified Plasmadynamics Model of a Coaxial Self-Field Plasma Accelerator3
Suppression of Azimuthal Combustion Instability Using Perforated Liner Under Symmetry Breaking3
Design Space Exploration of Lithium-Ion Battery Packs for Hybrid-Electric Regional Aircraft Applications3
Hall Thruster System Using Dry Ice Propellant at the Triple Point3
Announcements and Acknowledgments3
Parameter Influence on Porous Bleed Performance for Supersonic Turbulent Flows3
Stochastic Equilibrium Analysis to Optimize Solid Propellant Combustion Gas Composition3
Combined Cycle Nuclear System Architecture for Crewed Mars Spacecraft Propulsion and Power3
Plasma–Wall Interaction Model for Erosion of Materials Under Ion Bombardment3
Charactering Catalytic Ignition and Combustion for the Ninety-Percent Hydrogen-Peroxide/Paraffin-Based Hybrid Rocket Engine3
Development of a Liquid-Propellant Rocket Powered by a Rotating Detonation Engine3
Variably Premixed Rotating Detonation Engine for Evaluation of Detonation Cycle Dynamics3
Development and Evaluation of Reduced Kinetics Models for 1,3-Butadiene–Air Combustion3
Novel Solid Propellants Enabled Through In Situ Martian Perchlorates3
Data-Driven Analysis of Tortuous Gas Turbine Inlet Truncation to Reduce Computational Cost3
Limit Cycle Oscillating Detonation Wave Behavior Analysis Within a Rotating Detonation Engine3
Design of an Internal Osculating Waverider Intake3
Microthrusters’ Combustion Control Using Jellied Propellant Flowing Through an Orifice Plate3
Study of Boron Fuel in a Water-Breathing Ramjet3
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