Journal of Propulsion and Power

Papers
(The TQCC of Journal of Propulsion and Power is 4. 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 2022-01-01 to 2026-01-01.)
ArticleCitations
Experimental Characterization of a Hollow Cathode with Iridium–Cerium Alloy25
Announcements and Acknowledgements22
Prediction of Burning Characteristics of Dihydroxyglyoxime Composite Propellant20
Expandable Graphite, a Novel Regression Rate Enhancer in the Solid Fuel Ramjet19
Correlation for Restart Boundaries of Simplified Two-Dimensional Hypersonic Inlets18
Combined Heat Shield and Solar Thermal Propulsion System for an Oberth Maneuver18
Numerical Simulations of Fuel Shape Change in Paraffin–Oxygen Hybrid Rocket Engines17
Detailed Performance Studies on a Small Electric-Powered Contra-Rotating Ducted Fan Engine16
Overview of Selected Serpentine Duct Simulations Using Computational Fluid Dynamics15
Effect of Co- and Counterswirl Air on Swirl Airblast Atomization15
Direction Control of Rotating Detonation Waves with Helical Combustion Chambers14
Preparation, Ignition, and Combustion of Boron Fuels with CuO as an Additive14
Simulation of Vacuum Chamber Pressure Distributions with Uncertainty Quantification13
Firing Tests and Simulations of a CubeSat-Scale H2O2-Based Hybrid Rocket12
Acoustic Waves Generated in Hypergolic Drop Tests of Low- and High-Volatility Fuels12
Combustion of 3D Printable Hybrid Rocket Fuels11
Dynamic Regulation Process of the Variable-Geometry Power Turbine10
Data-Driven Wall Pressure Reconstruction and Sparse Sensor Optimization for Supersonic Nozzles10
Characterizing Hypergolic Propellants Using Impinging Jets and Droplets in Acoustic Levitation10
Stochastic Emission in Passively Fed Single-Emitter Porous-Media Ionic Liquid Ion Sources9
Driving Mechanisms in Low-Order Modeling of Longitudinal Combustion Instability9
Numerical and Experimental Study of an Aircraft Igniter Plasma Jet Discharge9
Family of Skeletal Reaction Mechanisms for Methane–Oxygen Combustion in Rocket Propulsion9
General Burnback Analysis for Anisotropic and Heterogeneous Solid Propellants9
Multi-Element Gaseous Methane–Oxygen Rocket Combustor Optimization for Modern Space-Flight Technology9
Loss Mechanisms of Shrouded Stator Cavity Flow in an Axial Compressor8
Operation and Power Generation of a Disk-Shaped Pressure Gain Combustor8
Effect of Varying Secondary Swirl Injector Location on Performance of Hybrid Rocket8
Effects of Thermal/Chemical Nonequilibrium on a High-Mach Ethylene-Fueled Scramjet8
Advancing Mistuning Identification and Dynamic Modeling of Blisks Through Blade Detuning Tests8
Active Flow Control in Compressor Cascades with Steady and Pulsed Jets8
Machine-Learning-Based Rotating Detonation Engine Diagnostics: Evaluation for Application in Experimental Facilities8
Contribution of Unsteadiness to Solid Fuel Burning Characteristics in a Scramjet Combustor8
Performance of Novel Electrode Structures for Electrically Controlled Solid Propellant7
Fully Coupled Analysis of Aerothermoelastic Deformation of a Scramjet Inlet7
Multipoint Aerodynamic Optimization of Three-Dimensional Ultra-High-Bypass-Ratio Engine Intakes7
Experimental Investigation on Atomization of JP-10 Slurry Jets Containing Boron Nanoparticles7
Pilot Injection Impact on Ignition of F-24/ATJ Blends Under Various Conditions7
Surface Structure of Reacting Solid Ramjet Fuels7
Experimental Investigation of Throttleable H2O2 and Polypropylene Hybrid Rocket Motor7
Thermal and Resonance Characteristics of Tapered Cavities of Various Lengths7
Uncertainty Quantification of Slab Burner Simulation: Surrogates, Forward Propagation, and Parameter Calibration7
Effect of Fuel Injection Strategy on Generic Scramjet Combustor Operation7
Effects of Evaporation Modeling on Kerosene–Air Oblique Detonation7
Crossflow Decane Combustion Using Catalytically Decomposed High-Test Peroxide6
Injection Temperature and Scheme Effects on Neutral Flow Dynamics in Hall Thrusters6
Thermal–Combustion Coupled Instability in Hybrid Rockets with Fuel Blowing6
Improved Hybrid Rocket Performance by Additively Manufactured Gel-Infused Solid Fuels6
Fundamental Experiment and Numerical Simulation of Ne/Xe Plasma Magnetohydrodynamic Electrical Power Generation6
Numerical Modeling to Investigate the Aerodynamics of a Boundary-Layer Ingested Transonic Fan6
Experimental Investigation on Aluminum-Based Water Ramjet for Propelling High-Speed Underwater Vehicles6
Impact of Ammonium Perchlorate Content on Electrically Controlled Gel Polymer Electrolyte Monopropellants6
Evaluation of Radiative Heat-Transfer Effect on Paraffin-Wax Regression Rate in Hybrid Rocket6
Interaction Behavior of Pulsejet Engines6
Supersonic Combustion and Flow Evolution in Dual-Combustion Ramjet Engine5
Delayed Detached-Eddy Simulations of Rough-Wall Turbulent Reactive Flows in a Supersonic Combustor5
Design of an Internal Osculating Waverider Intake5
Radial Mass Flow Rate Partition on LOx/GCH4 Pintle Injector Configurations5
Numerical Turbulence Modeling in a Transonic Boundary-Layer Ingestion Intake5
Wave Detection and Tracking Within a Rotating Detonation Engine Through Object Detection5
Fuel Regression Characteristics of Axial-Injection End-Burning Hybrid Rockets Using LOX5
Beam Misalignment Effects on Microwave Rocket Propulsion Performance5
Computational Analysis and Regression Laws for Nozzle Erosion Prediction in Hybrid Rockets5
Unraveling the Transition from Standard to Reactive Atomization of Hypergolic Propellants5
Impact of Future Low-Emissions Combustor Technology on Acoustic Scaling Laws5
Low-Order Autoignition Modeling for Hydrogen Transverse Jets5
High-Specific-Impulse Electrospray Propulsion with Small Capillary Emitters4
Novel Solid Propellants Enabled Through In Situ Martian Perchlorates4
Combined Cycle Nuclear System Architecture for Crewed Mars Spacecraft Propulsion and Power4
Limit Cycle Oscillating Detonation Wave Behavior Analysis Within a Rotating Detonation Engine4
Parametric Analysis of Hydrogen Swirl Combustors with Incompletely Stirred Reactor Network Modeling4
Data-Driven Analysis of Tortuous Gas Turbine Inlet Truncation to Reduce Computational Cost4
Design and Performance of an Electrowetting Ionic Liquid Electrospray Thruster Prototype4
Suppression of Azimuthal Combustion Instability Using Perforated Liner Under Symmetry Breaking4
Design Space Exploration of Lithium-Ion Battery Packs for Hybrid-Electric Regional Aircraft Applications4
Computationally Examining the Effect of Plate Thickness on Hole-Emitter-Type Electrospray Thrusters4
Control of Shock-Induced Flow Separation Using Rectangular Air-Jet Vortex Generators4
Simplified Plasmadynamics Model of a Coaxial Self-Field Plasma Accelerator4
Plasma–Wall Interaction Model for Erosion of Materials Under Ion Bombardment4
Stochastic Equilibrium Analysis to Optimize Solid Propellant Combustion Gas Composition4
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