Journal of Propulsion and Power

(The TQCC of Journal of Propulsion and Power is 2. 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 2020-07-01 to 2024-07-01.)
Numerical Analysis of Paraffin-Wax/Oxygen Hybrid Rocket Engines24
Experimental Study of a Hypergolically Ignited Liquid Bipropellant Rotating Detonation Rocket Engine21
Penetration and Combustion Studies of Tandem Liquid Jets in Supersonic Crossflow12
Increased Thrust-to-Power Ratio of a Stepped-Diameter Helicon Plasma Thruster with Krypton Propellant10
Experimental Studies of Ice Crystal Accretion on Axisymmetric Bodies at Aeroengine Conditions9
Development of a Liquid-Propellant Rocket Powered by a Rotating Detonation Engine9
Statistics and Dynamics of Intermittent Boundary Layer Flashback in Swirl Flames8
Diode Laser Ignition Mechanism for Hybrid Propulsion Systems7
Effects of Groove Structure on Spray Characteristics of a Throttleable Pintle Injector6
Variably Premixed Rotating Detonation Engine for Evaluation of Detonation Cycle Dynamics6
Flame Dynamics in an Optically Accessible Solid Fuel Ramjet Combustor6
Thrust Performance of Converging Rotating Detonation Engine Compared with Steady Rocket Engine5
Regression and Flame Structure in Cavity Flameholding Solid-Fuel Ramjet Fuel Grains5
Control of Large-Amplitude Combustion Oscillations Using Nanosecond Repetitively Pulsed Plasmas5
Flame Dynamics in the Combustion Chamber of Hybrid Rocket Using Multiangle Chemiluminescence5
Explicit Analytical Equations for Single Port Hybrid Rocket Combustion Chamber Sizing5
Decomposition of Ammonium-Perchlorate-Encapsulated Nanoscale and Micron-Scale Catalyst Particles4
Design of an Internal Osculating Waverider Intake4
Equivalent Supply Pressure for Pressure Gain Estimation in Rotating Detonation Engines4
Effects of Thermal/Chemical Nonequilibrium on a High-Mach Ethylene-Fueled Scramjet4
Experimental Investigation on Aluminum-Based Water Ramjet for Propelling High-Speed Underwater Vehicles4
Role of Precombustion Chamber Design in Feed-System Coupled Instabilities of Hybrid Rockets4
Rheological, Ballistic, and Mechanical Properties of 3D Printed, Photocured Composite Propellants4
Experimental Investigation of Throttleable H2O2 and Polypropylene Hybrid Rocket Motor3
Numerical Estimation of Nozzle Throat Heat Flux in Oxygen-Methane Rocket Engines3
Pulsed Electrogasdynamic Thruster for In-Space Propulsion3
Propellant Surface Evolution of a Coaxial Pulsed Plasma Thruster3
Uncertainty and Sensitivity Analysis of Bleed Modeling in Shock/Turbulent Interactions3
Simulated Scramjet Shock Train Control Using an All-Coefficient Adaptive Control Approach3
Iodine Electric Propulsion System Thrust Validation: From Numerical Modeling to In-Space Testing3
Scramjet Engine Flowpath That Improves Specific Impulse Using JP-7 Fuel3
Impact of Design Constraints on Noise and Emissions of Derivative Supersonic Engines3
Operation of a High-Power Nested Hall Thruster with Reduced Cathode Flow Fraction3
Ozone-Enhanced Flame Propagation of Methane/Ethylene/Air Mixtures at Subatmospheric Pressures3
Numerical Simulations of Fuel Shape Change in Paraffin–Oxygen Hybrid Rocket Engines3
Ignition and Extinction Characteristics of Electrically Controlled Solid Propellants2
Conceptual Design of a Space Power System Based on Combustion of Metals2
Extinguishing and Combustion Characteristics of Electrically Controllable Solid Propellants Under Elevated Pressures2
Mechanisms Contributing to the Dynamic Stability of a Flexible Subscale Rocket Nozzle2
Transient, Multiscale, Heterogeneous Model of Hydrogen Peroxide Decomposition for 3D-Printed Catalysts2
Increasing Burning Rate and Motor Thrust by Expandable Graphite Additives2
Flow Development in Radial Plane of Rotating Detonation Engine Integrated with Aerospike2
Coupling Effect of Multicavity on Flame Stabilization Mode Transitions in Scramjet Combustor2
Novel Hypergolic Green Fuels with Hydrogen Peroxide for Propulsion Systems2
Investigating the Chemical Stability of Electrospray Plumes During Particle Collisions2
Wave Detection and Tracking Within a Rotating Detonation Engine Through Object Detection2
Three-Dimensional Kinetic Simulations of Carbon Backsputtering in Vacuum Chambers from Ion Thruster Plumes2
Improved Hybrid Rocket Performance by Additively Manufactured Gel-Infused Solid Fuels2
Design Space Exploration of Lithium-Ion Battery Packs for Hybrid-Electric Regional Aircraft Applications2
Active Flow Control in Compressor Cascades with Steady and Pulsed Jets2
Unsteady Stream-Tube Model for Pulse Performance of Bipropellant Thrusters2
Driving Mechanisms in Low-Order Modeling of Longitudinal Combustion Instability2
Parameter Influence on Porous Bleed Performance for Supersonic Turbulent Flows2
Performance Comparison of Paraffin/Ethanol Fuel Blends in a Laboratory-Scale Hybrid Rocket Motor2
Numerical Performance Analysis of a Supersonic Combustor at Mach 8 Flight Off-Design Conditions2