This Journal is devoted to the advancement of the science and technology of aerospace propulsion and power through the dissemination of original archival papers contributing to advancements in airbreathing, electric, and advanced propulsion; solid and liquid rockets; fuels and propellants; power generation and conversion for aerospace vehicles; and the application of aerospace science and technology to terrestrial energy devices and systems. It is intended to provide readers of the Journal, with primary interests in propulsion and power, access to papers spanning the range from research through development to applications. Papers in these disciplines and the sciences of combustion, fluid mechanics, and solid mechanics as directly related to propulsion and power are solicited.
本杂志致力于通过传播对吸气式、电力和先进推进系统的进步作出贡献的原始档案文件，促进航空航天推进和动力的科学和技术的进步;固体和液体火箭;燃料和推进剂;航空航天器的发电和转换;以及将航空航天科学和技术应用于地面能源装置和系统。它旨在为主要关注推进和动力的读者提供从研究到开发再到应用的论文。在这些学科和燃烧科学，流体力学和固体力学的论文直接涉及推进和动力征集。
Two-Hundred-Newton Laboratory-Scale Hybrid Rocket Testing for Paraffin Fuel-Performance Characterization
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37017
Characterization of the Hypergolic Ignition Delay of Ammonia Borane
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37075
Electric solid propellant ablation in an arc discharge
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37517
Fundamental Scramjet Combustion Experiments Using Hydrocarbon Fuel
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37472
Single-Phase Instability in Non-Premixed Flames Under Liquid Rocket Engine Relevant Conditions
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37395
Aging Effects on the Burning Rates of Composite Solid Propellants with Nano-Additives
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37189
Background Pressure Effects on Ion Velocity Distributions in an SPT-100 Hall Thruster
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37133
Injector-Driven Flame Dynamics in a High-Pressure Multi-Element Oxygen–Hydrogen Rocket Thrust Chamber
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37406
Role of Ignition Delay in Rotating Detonation Engine Performance and Operability
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37117
10000-Ignition-Cycle Investigation of a LaB6 Hollow Cathode for 3–5-Kilowatt Hall Thruster
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37192
High Pressure Fuel Regression Characteristics of Axial-Injection End-Burning Hybrid Rockets
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37135
Influences of Domain Symmetry on Supersonic Combustion Modeling
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37227
Advancing the Microcathode Arc Thruster: Effect of the Ablative Anode
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37145
Aluminum Combustion Can Drive Instabilities in Solid Rocket Motors: T-Burner Study
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37034
Development of Kinetic Models for the Hybrid Fuels Combustion Containing Aluminum Particles
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37201
Optical Diagnostics in a High-Pressure Combustor with Gaseous Oxygen and Kerosene
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37050
Lithium-Perchlorate/Polyvinyl-Alcohol-Based Aluminized Solid Propellants with Adjustable Burning Rate
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37279
Development of a Skeletal Mechanism for Aviation Kerosene Surrogate Fuel
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37421
Dynamics of a Small-Scale Hydrogen Peroxide Vapor Propulsion System
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37323
Aluminum Oxide–Supported Manganese Oxide Catalyst for a 98% Hydrogen Peroxide Thruster
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37359
Utility of Multiprotrusion as the Performance Enhancer in Hybrid Rocket Motor
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37491
Flame Structure and Dynamics in a Premixed Dual-Mode Scramjet Combustor from Fluorescence Imaging
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37057
Characteristics of Ion–Ion Thruster Generating Continuously Positive and Negative Ion Beams
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37166
Deflagration-to-Detonation Transition in Nitrous Oxide/Oxygen-Fuel Mixtures for Propulsion
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37391
Systematic Measurement of Hydrocarbon Fuel Droplet Burning Rate Constants and Ignition Delays
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37195
Modification of Eigenmodes in a Cold-Flow Rocket Combustion Chamber by Acoustic Resonators
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37405
Radiation Heating Effects on Oxidizer-to-Fuel Ratio of Additively Manufactured Hybrid Rocket Fuels
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37037
Altering Agglomeration in a Composite Propellant with Aluminum-Silicon Eutectic Alloy
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37231
Vorticoacoustic Stability of Solid Rocket Motors: A Numerical Study
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37384
Numerical Investigations of S-Shaped Air Inlet for Embedded Engines
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37256
Characteristics of Gas-Centered Swirl-Coaxial Injector with Liquid Flow Excitation
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B36647
Turbulence Modeling Effects on Fuel Regression Rate in Hybrid Rocket Numerical Simulations
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.b37528
Biphasic Dispersion Fuels for High-Regression-Rate Hybrid Rockets
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37431
Parallel Large-Eddy Simulation of Subsonic and Transonic Flows with Transition in Compressor Cascade
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.b37371
Ballistic Performance of Paraffin-Based Solid Fuels Enhanced by Catalytic Polymer Degradation
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B36977
Characterization of Rotating Detonation Engine Injector Response Using Laser-Induced Fluorescence
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37309
Data-Driven One-Dimensional Modeling of Pseudoshocks
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37175
Impulse Generation and Stabilization Performance of a Doughnut–Spherical Laser Launch System
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37442
Temperature and Size Measurements of Cryogenic Spray Droplets with Global Rainbow Refractometry
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B36750
Simplified Description of Heat Release Oscillations for Assessing Combustor Stability
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B36740
Numerical Investigations on Oscillating Aspiration Control in High-Load Compressor Cascades
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37200
Propellant Atomization for Porous Injectors
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.b37569
Identifying Weaknesses in Eddy-Viscosity Models for Predicting Film Cooling via Large-Eddy Simulations
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37314
Numerical Simulation of Two-Phase Flow Within Aerated-Liquid Injectors
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37284
Deposit Formation and Heat Transfer for Bioethanol-Fueled Rocket Engine Combustion Chamber Liners
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B36887
Reduced Order Modeling of a Supersonic Flow Field
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37064
Hot Streak Characterization of High-Performance Double-Serpentine Exhaust Nozzles at Design Conditions
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37235
Demonstration of Thrust Vector Control by Hydrogen Peroxide Injection in Hybrid Rockets
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37074
Linear Acoustic Analysis of the Preburner of an Oxidizer-Rich Staged Combustion Engine
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B37132
Computational Study of Combustor Dilution Flow Interaction with Turbine Vanes
来源期刊：Journal of Propulsion and PowerDOI：10.2514/1.B36912
