Dr. Toru Shimada
Current affiliation: Japan Aerospace Exploration Agency
Subject: Astronautics
Primary location: Japan
Liquid Films Instability Analysis of Liquefying Hybrid Rocket Fuels Under Supercritical Conditions
Published in:AIAA Journal
Publication date:2015-06-01
Instability Analysis of Liquid Films of Liquefying Hybrid Rocket Fuels under Supercritical Operating Condition
Published in:52nd Aerospace Sciences Meeting
Publication date:2014-01-10
Numerical Simulations of Combustive Flows in a Swirling-Oxidizer-Flow-Type Hybrid Rocket
Published in:52nd Aerospace Sciences Meeting
Publication date:2014-01-10
Linear Combustion Stability Analysis of Uni-directional Vortex Injection Hybrid Rocket Engines
Published in:50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Publication date:2014-07-25
Combined Analysis of Reactive Flow and Heat Transfer for Hybrid Rocket Design Engineering
Published in:50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Publication date:2014-07-25
Agglomeration characteristics of aluminum particles with changing pressure in AP/AN composite propellants
Published in:50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Publication date:2014-07-25
Visualization of Flames in Combustion Chamber of Hybrid Rocket Engine with Multi-Section Swirl Injection Method
Published in:50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Publication date:2014-07-25
Study on Hybrid Rocket with Multi-Section Swirl Injection Method toward Flight Experiments of Subscale Space Plane
Published in:50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Publication date:2014-07-25
Flight Performance Simulations of Vertical Launched Sounding Rockets Using Altering-Intensity Swirling-Oxidizer-Flow-Type Hybrid Motors
Published in:51st AIAA/SAE/ASEE Joint Propulsion Conference
Publication date:2015-07-23
Investigation of Flight Profiles Suitable for Altering-Intensity Swirling-Oxidizer-Flow-Type Hybrid Rocket
Published in:51st AIAA/SAE/ASEE Joint Propulsion Conference
Publication date:2015-07-23
Numerical simulation of luminous flame around ignited aluminum particle near burning surface of composite propellant with changing pressure
Published in:51st AIAA/SAE/ASEE Joint Propulsion Conference
Publication date:2015-07-23
Ascendancy of Extinction-Reignition on Single-Stage Hybrid Sounding Rocket in View of Fuels
Published in:57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
Publication date:2016-01-01
Numerical Investigation of Roll Torque Induced by Solid Rocket Motor Internal Flow
Published in:Journal of Propulsion and Power
Publication date:2009-11-01
Experimental Study of an N2O/Ethanol Propulsion System
Published in:43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
Publication date:2007-07-08
Head-End Injected Swirling Gas Flow in a Chamber
Published in:45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
Publication date:2009-08-02
Numerical Simulation of Diffusion Combustion in a Turbulent Boundary Layer Considering Reaction Progression
Published in:46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
Publication date:2010-07-25
Regression Modeling of Paraffin-based Hybrid Rocket Fuels for Internal Ballistics Simulation
Published in:46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
Publication date:2010-07-25
Predictions of Nozzle Shape Change Using a Coupled Fluid/Thermochemical Approach
Published in:43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
Publication date:2007-07-08
Numerical Investigation of Roll Torque Induced by Solid Rocket Motor Internal Flow
Published in:44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
Publication date:2008-07-21
Study on Al/Al2O3 Agglomeration Particle Size Distributions for Solid Propellants
Published in:42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
Publication date:2006-07-09
Validation of Numerical Simulation of Swirling Turbulent Flow for Hybrid Rocket Research
Published in:47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
Publication date:2011-07-31
EXPERIMENTAL STUDY ON MIDWEB ANOMALY OF COMPOSITE PROPELLANT GRAINS
Published in:International Journal of Energetic Materials and Chemical Propulsion
Publication date:2009-01-01
Polymer Combustion as a Basis for Hybrid Propulsion: A Comprehensive Review and New Numerical Approaches
Published in:Energies
Publication date:2011-10-24
Large Eddy Simulation of Swirling Combustion Flow with Wall Fuel Blowing modeled for Hybrid Rocket Engines
Published in:49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Publication date:2013-07-12
Model of Hybrid Rocket Combustion in Classical Hybrid Rocket Motors
Published in:49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Publication date:2013-07-12
CHARACTERISTICS OF CHEMICALLY MODIFIED AND NANOCOMPOSITE POLYMERS AS NOVEL FUELS FOR HYBRID ROCKET PROPULSION
Published in:International Journal of Energetic Materials and Chemical Propulsion
Publication date:2012-01-01
Velocity and Temperature Distributions Around Metal Particles in the Reaction Zone of AP Composite Propellant
Published in:45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
Publication date:2009-08-02
Hot Gas Flow Around Burning Aluminum Particles Near Burning Surface of AP Composite Propellant
Published in:46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
Publication date:2010-07-25
Visualization of Flames in Combustion Chamber of Swirling-Oxidizer-Flow-Type Hybrid Rocket Engines
Published in:46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
Publication date:2010-07-25
A LINEAR STABILITY ANALYSIS OF OSCILLATORY COMBUSTION INDUCED BY COMBUSTION TIME DELAYS OF LIQUID OXIDIZER IN HYBRID ROCKET MOTORS
Published in:International Journal of Energetic Materials and Chemical Propulsion
Publication date:2014-01-01
A Study of Hybrid Rockets with Multi-Section Swirl Injection Method
Published in:48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
Publication date:2012-07-30
Evaluation of Ablation and Longitudinal Vortices in Solid Rocket Motor by Computational Fluid Dynamics
Published in:42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
Publication date:2006-07-09
Correlation of Midweb Anomaly with Microstructure of Composite Propellant Containing High Amount of Aluminum
Published in:47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
Publication date:2011-07-31
Solid propulsion for space applications: An updated roadmap
Published in:Acta Astronautica
Publication date:2010-01-01
COMBUSTION MECHANISM OF TETRA-OL GLYCIDYL AZIDE POLYMER AND ITS APPLICATION TO HYBRID ROCKETS
Published in:International Journal of Energetic Materials and Chemical Propulsion
Publication date:2009-01-01
A Study on Performance Improvement of Paraffin Fueled Hybrid Rocket Engines with Multi-Section Swirl Injection Method
Published in:49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Publication date:2013-07-12
Effects of Multi-Section Swirl Injection Method on Fuel Regression Rate of High Density Polyethylene Fueled Hybrid Rocket Engine
Published in:49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Publication date:2013-07-12
Validation with experiments on simplified numerical prediction of hybrid rocket internal ballistics
Published in:Not available
Publication date:2012-01-01
On assessment of numerical methods for diffusion-combustion flow with fast chemistry
Published in:Not available
Publication date:2012-01-01
X-Ray Visualization Measurement of Slurry Flow in Solid Propellant Casting
Published in:AIP Conference Proceedings
Publication date:2007-01-01
Multidisciplinary Design Exploration for Sounding Launch Vehicle using Hybrid Rocket Engine in View of Ballistic Performance
Published in:International Journal of Turbo and Jet Engines
Publication date:2015-01-01
Conceptual Design of Single-Stage Launch Vehicle with Hybrid Rocket Engine for Scientific Observation Using Design Informatics
Published in:Journal of Space Engineering
Publication date:2013-01-01
Validation of Integral Method for Numerical Prediction of Hybrid Rocket Internal Ballistics
Published in:Journal of Fluid Science and Technology
Publication date:2013-01-01
Low-Frequency Feed-System-Coupled Combustion Instability in Hybrid Rocket Motors
Published in:Journal of Thermal Science and Technology
Publication date:2013-01-01
Numerical Evaluation of Hybrid Rocket Internal Ballistics with Thermal Radiation Effect
Published in:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES AEROSPACE TECHNOLOGY JAPAN
Publication date:2014-01-01
Conceptual design: Dependence of parameterization on design performance of three-stage hybrid rocket
Published in:Journal of Fluid Science and Technology
Publication date:2014-01-01
Numerical analysis of multi-parallelized swirling flow inside a circular pipe
Published in:Journal of Mechanical Science and Technology
Publication date:2015-03-01
Multi-disciplinary Conceptual Design Knowledge of Multi-stage Hybrid Rocket Using Data Mining Technique
Published in:Journal of Mechanics Engineering and Automation
Publication date:2015-01-28
Diversity of design knowledge for launch vehicle in view of fuels on hybrid rocket engine
Published in:Journal of Advanced Mechanical Design Systems and Manufacturing
Publication date:2014-01-01
A Theoretical Study of Combustion Stability in Vortex Injection Hybrid Rocket Engine
Published in:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES AEROSPACE TECHNOLOGY JAPAN
Publication date:2014-01-01
Hybrid Rocket Performance Prediction with Coupling Method of CFD and Thermal Conduction Calculation
Published in:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES AEROSPACE TECHNOLOGY JAPAN
Publication date:2012-01-01
Flow Inside a Solid Rocket Motor with Relation to Nozzle Inlet Ablation
Published in:AIAA Journal
Publication date:2007-06-01
Solid-Fuel Regression Rate for Standard-Flow Hybrid Rocket Motors
Published in:Journal of Thermal Science and Technology
Publication date:2012-01-01
Experimental Investigation on Microwave Interference in Full-Scale Solid Rocket Exhaust
Published in:Journal of Spacecraft and Rockets
Publication date:2010-07-01
Design optimization of launch vehicle concept using cluster hybrid rocket engine for future space transportation
Published in:Journal of Fluid Science and Technology
Publication date:2016-01-01
Evolutionary algorithm applied to ballistic launch vehicle design using hybrid rocket engine evaluated by enhanced flight simulation
Published in:2015 IEEE Congress on Evolutionary Computation (CEC)
Publication date:2015-05-01
Stability Analysis of Solid Rocket Motor Combustion by Computational Fluid Dynamics
Published in:13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference)
Publication date:2007-05-21
Computational fluid dynamics in the design of M-V launch vehicle
Published in:34th Aerospace Sciences Meeting and Exhibit
Publication date:1996-01-15
Numerical Analysis of Flow Inside a Solid Rocket Motor with Relation to Nozzle Inlet Ablation
Published in:36th AIAA Fluid Dynamics Conference and Exhibit
Publication date:2006-06-05
Correlation of Midweb Anomaly with Microstructure of Composite Propellant
Published in:AIAA Guidance, Navigation, and Control Conference
Publication date:2010-08-02
Computation of HYFLEX aerodynamic heating at HEK shock-tunnel test conditions
Published in:33rd Thermophysics Conference
Publication date:1999-06-28
CFD ANALYSES OFLOW FREQUENCYCOMBUSTION INSTABILITYIN SOLID PROPELLANT ROCKET MOTORS
Published in:International Journal of Energetic Materials and Chemical Propulsion
Publication date:2007-01-01
ロケットノズル材料の熱拡散率評価
Published in:Netsu Bussei
Publication date:2003-01-01
Visualization and Emission Spectra of Flames in Combustion Chamber of Swirling-Oxidizer-Flow-Type Hybrid Rocket Engines
Published in:Journal of Thermal Science and Technology
Publication date:2011-01-01
Conceptual Design of Single-Stage Launch Vehicle with Hybrid Rocket Engine Using Design Informatics
Published in:Computational Methods in Applied Sciences
Publication date:2014-11-15
Advanced Computer Science on Internal Ballistics of Solid Rocket Motors
Published in:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES AEROSPACE TECHNOLOGY JAPAN
Publication date:2010-01-01
Tetra-ol Glycidyl Azide Polymer Combustion Modeling
Published in:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES SPACE TECHNOLOGY JAPAN
Publication date:2009-01-01
Experimental Study of Fragmentation of Hybrid Rocket Fuel
Published in:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES AEROSPACE TECHNOLOGY JAPAN
Publication date:2014-01-01
設計情報学を用いたハイブリッドロケットエンジン搭載単段式宇宙輸送機の概念設計
Published in:Transactions of the JSME (in Japanese)
Publication date:2014-01-01
Low-Frequency Combustion Instability Induced by the Combustion Time Lag of Liquid Oxidizer in Hybrid Rocket Motors
Published in:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES AEROSPACE TECHNOLOGY JAPAN
Publication date:2012-01-01
Multi-Stage Hybrid Rocket Conceptual Design for Micro-Satellites Launch using Genetic Algorithm
Published in:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
Publication date:2012-01-01
A test of equivalence of the variable-hard-sphere and inverse-power-law models in the direct-simulation Monte Carlo method
Published in:Physics of Fluids A Fluid Dynamics
Publication date:1991-01-01
Investigation of Microwave Attenuation by Solid Rocket Exhausts
Published in:47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition
Publication date:2009-01-05
Implicit LES of Compressible Turbulent Flow over a Backward-Facing Step in the Nozzle of Solid Rocket Motor
Published in:48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
Publication date:2010-01-04
Active debris multi-removal mission concept based on hybrid propulsion
Published in:Acta Astronautica
Publication date:2014-10-01
Improvement of Regression Rate and Combustion Efficiency of High Density Polyethylene Fuel and Paraffin Fuel of Hybrid Rockets with Multi-Section S...
Published in:47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
Publication date:2011-07-31
MODIFIED BURNING RATE SPECTRUM & COMBUSTION MECHANISM OFTETRA-OLGAP
Published in:International Journal of Energetic Materials and Chemical Propulsion
Publication date:2007-01-01
A210 2方向からのX線撮影によるスラリーの流れの可視化
Published in:Journal of the Visualization Society of Japan
Publication date:2006-01-01
Combustion of Aluminum Particles near Burning Surface of Composite Propellant
Published in:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
Publication date:2011-01-01
Conceptual Design of Single-Stage Hybrid Rocket for Scientific Observation in View of Fuels Using Design Informatics
Published in:AEROSPACE TECHNOLOGY JAPAN THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
Publication date:2014-01-01
Static Burning Tests on a Bread Board Model of Altering-intensity Swirling-Oxidizer-Flow-Type Hybrid Rocket Engine
Published in:52nd AIAA/SAE/ASEE Joint Propulsion Conference
Publication date:2016-07-22
Quasi 1-D Numerical Analysis of Combustion Instability in Hybrid Rocket Motor Incorporating Boundary Layer Lags
Published in:52nd AIAA/SAE/ASEE Joint Propulsion Conference
Publication date:2016-07-22
Effective Operations of Extinction-Reignition with Simple Control of Oxidizer Flux on a Single-Stage Sounding Hybrid Rocket
Published in:19th AIAA Non-Deterministic Approaches Conference
Publication date:2017-01-05
Performance and Regression Rate Characteristics of 5-kN Swirling-Oxidizer-Flow-Type Hybrid Rocket Engine
Published in:Journal of Propulsion and Power
Publication date:2017-07-01