March 17, 2016.Room Room A Room B Room C Room D Room E

SessionChair

Co-Chair

A-1:Jet Engine 1Mizuho Aotsuka (IHI)

B-1:OS Acoustics in Propulsion SystemsSusumu Teramoto (The University of Tokyo)

Seiji Tsutsumi (JAXA)

C-1: Combustion AcousticsJaye Koo (Korea Aerospace University)

D-1:PropellantTakeshi Kanda (JAXA)

Timothee L Pourpoint (Purdue University)

E-1:Cryogenic FuelYu Daimon (JAXA)

Soonsam Hong (KARI)

8:40～9:00 AJCPP2016-027 AJCPP2016-131 AJCPP2016-156 AJCPP2016-057Numerical Simulation of Sand Erosion Phenomenon ofCMC Coated Substrate Caused by Low SpeedParticles

Acoustic Research Programs in Aircraft Engines inJAXA: aFJR and Green Engine

Experimental Study on Liquid Core Length of SimulantGel with and without Nano-sized Metal Particles

Experimental Study on Sloshing with Phase Changeusing Liquid Nitrogen

Yoshimasa Fuma, Makoto Yamamoto, Hiroya Mamori(Tokyo University of Science), Yoji Okita (IHI)

Tatsuya Ishii, Kenichiro Nagai, Hideshi Oinuma, JunichiKazawa, Shunji Enomoto (JAXA), Tsutomu Oishi (IHI)

Kyehwan Kim, Seongjoo Han, Heejang Moon, JinkonKim (Korea Aerospace University)

Daichi Haba, Takehiro Himeno, Toshinori Watanabe,Chihiro Inoue, Seiji Uzawa (The University of Tokyo),Satoshi Nonaka, Yutaka Umemura(JAXA)

9:00～9:20 AJCPP2016-075 AJCPP2016-089 AJCPP2016-022 AJCPP2016-067Study on the Test Bench Development for the EECUPerformance Verification Test of Aircraft Gas TurbineEngine

Comparison of Acoustic Intensity Vectors with SPLand Phase Distributions of Supersonic Jet

Numerical Analysis of Exhaust Plume for 10N GradeMMH-NTO Thruster with Frozen Equilibrium

Study for numerical calculation of dynamic wetting inspacecraft propellant tank

Kho Seonghee, Ki Jayoung (EGT Co., Ltd), KongChangduk (Chosun University)

Masahito Akamine, Koji Okamoto (The University ofTokyo), Kent L. GeeGee, Tracianne B. Neilsen(Brigham-Young University), Susumu Teramoto (TheUniversity of Tokyo), Seiji Tsutsumi (JAXA), TakeoOkunuki (The University of Tokyo)

Hyeonah Kim, Kyun Ho Lee (Sejong University) Ryoji Imai, Yuji Amano, Sho Goto (Muroran Institute ofTechnology)

9:20～9:40 AJCPP2016-178 AJCPP2016-132 AJCPP2016-052 AJCPP2016-030 AJCPP2016-060Effect of the Axial Location of Single CircumferentialCasing Groove on the Unsteadiness of Tip LeakageFlow in a Transonic Compressor

Impact of Secondary Jets from a Partitioned AnnularSlit on Acoustics of Heated Subsonic Jet

Swirling Premixed Flame Response on TransverseAcoustic Excitation

Experimental investigation on the evaporation processof ADN-based liquid propellant

Numerical Simulation of Bubble Point Tests of MeshScreens for Use in Propellant Management Device

Xiaoyong Zhou, Qingjun Zhao, Weiwei Cui, Xiaolei Sun,Jing Li (Chinese Academy of Sciences)

Kanta Sato (The University of Tokyo), Tatsuya Ishii,Hideshi Oinuma, Kenichiro Nagai (JAXA), ShigehikoKaneko, Hirofumi Daiguji (The University of Tokyo)

Yongjin Park, Seonghyeon Seo (Hanbat NationalUniversity)

Liyue Jing, Jialong Huo, Xiaoqing You, Min Zhu(Tsinghua University), Zhaopu Yao (Beijing Institute ofControl Engineering)

Hyuntak Kim (KAIST), Sang Hyuk Lim, Hosung Yoon(Space Solutions Co. Ltd.), Sejin Kwon (KAIST)

9:40～10:00 AJCPP2016-058 AJCPP2016-127 AJCPP2016-010 AJCPP2016-036 AJCPP2016-175JAXA aeronautical programs and future aero engine Application of Linearized Euler Equation Solver in

Frequency Domain to Sound Propagation and RadiationProblems

Effects of Acoustic Forcing and Fuel Properties onVortex-Flame Interaction in a Dump Combustor

Development of Liquid Propellant Miniature MicrowaveDischarge Thruster

Study on Propellant Management Devices by Mesh-type Baffles

Hisao Futamura (JAXA) Sho Tokunaga, Yoshimi Nagayama, Yuzo Inokuchi,Nobuhiko Yamasaki (Kyushu University)

Donghyun Hwang, Kyubok Ahn (Chungbuk NationalUniversity)

Bunsuke Ueno, Hou-Yi Lee, Koichi Ushio, NaojiYamamoto, Taichi Morita, Hideki Nakashima (KyushuUniversity)

Shizuka Hamajima, Takehiro Himeno, Yasunori Sakuma,Toshinor Watanabe, Seiji Uzawa (The University ofTokyo), Yutaka Umemura, Hideyo Negishi (JAXA),Keitaro Ishikawa (Mitsubishi Heavy Industries)

10:00～10:20 AJCPP2016-189 AJCPP2016-122 AJCPP2016-056 AJCPP2016-182 AJCPP2016-051Effect of Viscosity and Surface Tension on the ImpactForce of Low-Speed DropletsColliding with a SolidSurface

Validation and Verification of Numerical PredictionMethod for Lift-off Acoustics of Launch Vehicles

Shock Attenuation in Gap Test Configuration forPyrotechnic Device

Performance Comparison of Catalysts on CommercialGrade Hydrogen Peroxide with Ethanol Blending

Development Study of a Capacitance Based VoidFraction Sensor for Cryogenic Two-phase Flow

Bin Zhang, Jingyin Li, Penghua Guo, Qian Lv ( Xi’anJiaotong University)

Seiji Tsutsumi, Keita Terashima (JAXA) Bohoon Kim, Minsung Kim, Jack J. Yoh (Seoul NationalUniversity)

Seungkwan Baek, Hongjae Kang, Woosuk Jung, SejinKwon (KAIST)

Yuki Sakamoto, Tetsuya Sato (Waseda University),Hiroaki Kobayashi (JAXA), Kota Uragaki, Shohei Tane,Kazuma Minote (Waseda University)

10:20～10:40SessionChair

Co-Chair

A-2:Rocket Engine TurbopumpMasaharu Uchiumi (JAXA)

Hiroumi Tani (JAXA)

B-2:OS Acoustics in Propulsion SystemsNobuhiko Yamasaki (Kyushu University)

Tatsuya Ishii (JAXA)

C-2:DetonationIn-Seuck Jeung (Seoul National University)

Ken Matsuoka (Nagoya University)

D-2:TurbineTetsuya Sato (Waseda University)

E-2:Space PropulsionYuya Oshio

(Tokyo University of Agriculture and Technology)

10:40～11:00 AJCPP2016-187 AJCPP2016-042 AJCPP2016-142 AJCPP2016-179 AJCPP2016-007The performance and cavitation research of high speedcentrifugal pump with the variable-pitch inducer

On the Prediction of Discrete Frequency NoiseGenerated by Fan and OGV Interaction in Aero-engine

Numerical Analysis of Oblique Detonation in FuelConcentration Gradients

Investigation on the Channel Boundary Optimization ofa Partial Admission Turbine

Theoretical Modeling and Simulation of FlyerAcceleration in Exploding Foil Initiator

Pei Chongyan, Li Linlin , Cheng Honggui (The 31stResearch Institute of CASIC), Sun Qiangqiang , LiYanhui , Yi Wanshuang , JIANG Jin (Wuhan University)

X. Wang, X. Sun (Beijing University of Aeronautics &Astronautics)

Kazuya Iwata, Shinji Nakaya, Mitsuhiro Tsue (TheUniversity of Tokyo)

Xiuming Sui, Wei Zhao, Qingjun Zhao, Weiwei Luo(Chinese Academy of Sciences)

Kyoungjin Kim, Ho Sang Kwak (Kumoh NationalInstitute of Technology), Kyu-Hyoung Kim (HanwhaCorporation), Seung-gyo Jang (Agency for DefenseDevelopment)

AJCPP2016-025 AJCPP2016-098 AJCPP2016-144 AJCPP2016-105 AJCPP2016-076Cavitation Characteristics of Small Turbopump forRocket Engine

Absorption Performance of Helmholtz Resonator madefrom Resin by 3D Printer

Numerical Investigation of Low Frequency Oscillationin Unsteady Shock-Induced Combustion over BluntProjectiles

DESIGN AND FLUID-THERMAL COUPLINGANALYSIS FOR A COOLING STRUCTURE OF A GASTURBINE VANE

Thrust Measurement of Magneto Plasma Sail combinedwith a Magnetic Nozzle.

Soonsam Hong, Changho Choi (KARI) Kei Kurihara, Yusuke Akamisaka, Kenta Kato, HidemiToh, Daisuke Sasaki (Kanazawa Institute ofTechnology), Tatsuya Ishii, Kenichiro Nagai (JAXA)

P.Pradeep Kumar, Kui-Soon Kim, Sejong Oh, Jeong-Yeol Choi (Pusan National University)

Zhang Wenting, Liu Hong (Tsinghua University) Yoshihiro Kajimura, Tatsumasa Hagiwara (AkashiNational College of Technology), Yoya Oshio, IkkohFunaki (JAXA), Hiroshi Yamakawa (Kyoto University)

11:00～11:20

Coffee Break

Room Room A Room B Room C Room D Room E11:20～11:40 AJCPP2016-083 AJCPP2016-019 AJCPP2016-155 AJCPP2016-053 AJCPP2016-112

Experimental Observation of Backflow-vortexCavitation on a Rotating Inducer

The Effect of Fuel Composition at Flame TransferFunction Characteristics of Partially PremixedCombustor

Structure of Rotating Detonation Waves in a Two-Parallel-Plane Combustor with Orthogonally MixingInjectors

Conjugate Heat Transfer Simulations ofTurbomachinery based on Discontinuous Galerkinmethod

Research and Development of High-Power Steady-State Magneto-Plasma-Dynamic Thrusters withPermanent Magnets for Manned Mars Exploration

Yutaka Ito, Takao Nagasaki (Tokyo Institute ofTechnology)

Jisu Yoon, Seongpil Joo, Jeongjin Kim, Youngbin Yoon(Seoul National University)

Soma Nakagami, Ken Matsuoka, Jiro Kasahara (NagoyaUniversity), Yoshiki Kumazawa, Jumpei Fujii, AkikoMatsuo (Keio University), Ikkoh Funaki (JAXA)

Longgang Liu, Chunwei Gu (Tsinghua University),Xiaodong Ren (Hong Kong University of Science andTechnology)

Kengo Chino, Kohei Kadohata, Tomoya Suzuki,Yoshikazu Sugiyama, Hirokazu Tahara, Kyoko Takada(Osaka Institute of Technology)

11:40～12:00 AJCPP2016-008 AJCPP2016-111 AJCPP2016-157 AJCPP2016-092 AJCPP2016-091Optimized Areodynamic Design of the Turbine for aRocket Turbopump

A Comparative Study on Aerodynamic Performanceand Noise Characteristics of Two Kinds of Long-earedOwl Wing Models Based on Different ReconstructionMethod

Experimental Flow Analysis of the Combustion ChannelFlow of a Rotating Detonation Engine

A numerical investigation of the unsteady flow field in asupersonic impulse turbine for swept rotor blade.

The time evolution of plasma and magnetic fieldstructure in a magnetic thrust chamber

Kazuyuki Yada, Noriyuki Shimiya, Masaharu Uchiumi(JAXA), Yuki Tokuyama, Ken-ichi Funazaki (IwateUniversity)

Dian Li, Luona Yang, Xiaomin Liu (Xi'an JiaotongUniversity)

Kazuki Ishihara, Yuichi Kato, Keisuke Goto, KenMatsuoka, Jiro Kasahara (Nagoya University),Yoshitaka Sato, Akiko Matsuo (Keio University), IkkohFunaki (JAXA)

Sooin Jeong, Byoungik Choi, Kuisoon Kim (PusanNational University)

Masafumi Edamoto, Naoya Saito, Taichi Morita, NaojiYamamoto, Ryosuke Kawashima, Hideki Nakashima(Kyushu University), Shinsuke Fujioka, Akifumi Yogo,Hiroaki Nishimura (Osaka University), Atsushi Sunahara(Institute for Laser Technology), Yoshitaka Mori (TheGraduate School for the Creation of New PhotonicsIndustries), Tomoyuki Johzaki (Hiroshima University)

AJCPP2016-138Compound sweep and lean effects of blade leadingedge on the performances of transonic centrifugalimpellers

Zhao Huijing , Wand Zhiheng , Tang Yonghong,Xi Guang(Xi'an Jiaotong University)

13:20～14:10

14:10～14:20

SessionChair

Co-Chair

A-3:OS Thrusters -propellant, internal phenomenonand development-

Chihiro Inoue (The University of Tokyo)

B-3:Fluid DynamicsKoji Okamoto (The University of Tokyo)

C-3: Scramjet and Ramjet 1Takayuki Kojima (JAXA)

D-3:Nano-Satellite PropulsionKyoungjin Kim

(Kumoh National Institute of Technology)Satoshi Hosoda (JAXA)

E-3:Solid Rocket PropulsionIchiro Nakagawa (Tokai University)

Kazuyuki Yada (JAXA)

14:20～14:40 AJCPP2016-038 AJCPP2016-170 AJCPP2016-009 AJCPP2016-113 AJCPP2016-043Development and Characterization of HypergolicPropellants at Purdue University

A Numerical Simulation of Transient Flow in a MissileCanister

Mach Number Effect on Breakdown of StreamwiseVortices in Supersonic Flow

Development of Osaka Institute of Technology Nano-Satellite PROITERES-2 with High-PowerElectrothermal Pulsed Plasma Thrusters

Numerical Simulation for Performance Prediction ofMEMS Solid Propellant Thruster

Timothee L Pourpoint (Purdue University) Bhushan A. Bhosale,, Seong Hun Bae, Jeong Soo Kim(Pukyong National University), Hyuk Soo Jeon, ChulHyun Park (Agency for Defense Development)

Yamato Tsukazaki, Shoji Sakaue, Takakage Arai (OsakaPrefecture University)

Hiroki Fujita, Tsubasa Yamauchi, Takuya Kamimura,Hirokazu Tahara, Kyoko Takada (Osaka Institute ofTechnology), Tomoyuki Ikeda (Tokai University)

Juyeong Jung (Hanbat National University), DaebanSeo (KARI), Jongkwang Lee (Hanbat NationalUniversity)

14:40～15:00 AJCPP2016-085 AJCPP2016-012 AJCPP2016-115 AJCPP2016-066Influence of downstream condition on the flow in sonicnozzle

Numerical Simulation of the Unsteady Flows inScramjet

Research and Development of Electrothermal PulsedPlasma Thrusters with High Total Impulse for the 2ndPROITERES Nano-Satellite

Extraction of detailed reaction kinetics of aluminizedRDX using isoconversional method and isothermal DSCfor propulsion

M M A Alam, Hideki Sato, Manabu Takao (NIT MatsueCollege), H D Kim (Andong National University),Toshiaki Setoguchi (Saga University)

Ruoyu Deng (Andong National University), Yingzi Jin(Zhejiang Sci-Tech University), Heuy Dong Kim(Andong National University)

Keita Kanaoka, Ryota Fujita, Koki Ryuho, Kohei Ono,Naoki Morikawa, Hirokazu Tahara, Kyoko Takada(Osaka Institute of Technology), Takashi Wakizono(High Serve Inc)

Yoocheon Kim, Jack J. Yoh (Seoul National University),Kuktae Kwon, Jungsu Park (Agency for DefenseDevelopment),

15:00～15:20 AJCPP2016-137 AJCPP2016-184 AJCPP2016-016 AJCPP2016-160 AJCPP2016-102Three-dimensional Flame Structure of Impinging GasJets for Space-craft Small Thrusters

A flow analysis of elbow intake duct for the purpose ofthe experiment of the turbo jet engine under the water

Vortex-Generator Control of the Supersonic Flow Pasta Cylindrical Protrusion

Experimental study on PTFE-sheet-fed pulsed plasmathruster

Rheological Study of Solid Ethanol Using DifferentSolidifying Agents

Yu Daimon, Hiroumi Tani (JAXA), Hiroshi Terashima(The University of Tokyo), Nozomu Kanno (MeijoUniversity), Yoshiki Matsuura (IHI Aerospace Co Ltd.),Mitsuo Koshi (Yokohama National University)

Gu Kim, Seonghee Kho, Jayoung Ki (EGT), YoungjunYu, Euntaek Lee (Agency for Defense Development)

Vignesh Ram P. Sethuraman (Andong NationalUniversity), Sudip Das (Birla Institute of Technology),Heuy Dong Kim (Andong National University)

Tetsushi Yoshikawa (Yokohama National University),Hitoshi Kuninaka (JAXA), Toru Hyakutake (YokohamaNational University), Kazutaka Nishiyama (JAXA)

Jerin John, Purushothaman Nandagopalan, Seung WookBaek (KAIST)

12:20～13:20

12:00～12:20

Lunch time

Coffee break

Room A L-1:Plenary Lecture Prof. Mitsuhiro Tsue (The University of Tokyo)

AJCPP2016-S01

National Flagship Launch System in the next generation, H3

Mr. Koichi Okita (JAXA)

Room Room A Room B Room C Room D Room E15:20～15:40 AJCPP2016-134 AJCPP2016-177 AJCPP2016-166 AJCPP2016-108

Numerical Modeling of Droplet Burning Rate ofHypergolic Propellants

Experimental Research on Aerated-Liquid Jet at LowGas-Liquid Ratio

Potential Measurement of a Plasma and a Thruster in aMiniature Microwave Discharge Plasma Thruster

Effect of the combustion instability on internal ballisticof Solid Rocket Motors

Hiroumi Tani, Yutaka Umemura, Yu Daimon (JAXA),Hiroshi Terashima (Hokkaido University), Mitsuo Koshi(Yokohama National University)

Zhang Wanzhou, Yang Shunhua, Le Jialing, DengWeixin, Tian Ye (China Aerodynamics Research andDevelopment Center)

Koichi Ushio, Bunsuke Ueno, Naoji Yamamoto, TaichiMorita, Hideki Nakashima (Kyushu University)

Ji-Seok Hong, Hong-Gye Sung, Heejang Moon (KoreaAerospace University), Won-Suk Ohm (YonseiUniversity), Seonghyeon Seo (Hanbat NationalUniversity), Dohyung Lee (Agency for DefenseDevelopment)

15:40～16:00 AJCPP2016-173 AJCPP2016-026Development of a low-power cylindrical type Hallthruster with permanent magnets for micro-satellites

Effect of Pintle on Low-Frequency L-star Instability inSolid Rocket Motors with Variable Pintle Thruster

Holak Kim, Seunghun Lee, Youbong Lim, Wonho Choe(KAIST)

Donghee Lee, Seongmin Joo, Junseong Kim,Seunghyun Ryu (Korea Aerospace University), HonggyeSung ,Heejang Moon, Juneseo Yang (Agency forDefense Development)

16:00～16:20

SessionChair

Co-Chair

A-4:OS Thrusters -propellant, internal phenomenonand development-

Jun Hayashi (Osaka University)

B-4:Jet Engine Compressor TechnologyKong Changduk (Chosun University)

Yasunori Sakuma (The University of Tokyo,)

C-4: Hypersonic Transport Propulsion 1Takakage Arai (Osaka Prefecture Uninersity)Heuy Dong Kim (Andong National University)

D-4:Non-Chemical PropulsionYoshihiro Kajimura

(Akashi National College of Technology)

E-4:Hybrid Rocket 1Takashi Sakurai (Tokyo Metropolitan University)

16:20～16:40 AJCPP2016-055 AJCPP2016-034 AJCPP2016-073 AJCPP2016-117 AJCPP2016-124Chemical kinetics of hypergolic ignition forCH3NHNH2/N2O4/NO2 gas mixtures

A New Method of Controlling Oscillation of CascadeBlades Based on a Genuine Three-dimensional Model

Dynamic Simulation of Hypersonic Pre-CooledTurbojet Engine

Thermal Design of Fully-Radiation-Cooled High-PowerSteady-State MPD Thrusters with Permanent Magnetsfor In-Space Propulsion

Experiments of an Ejector-jet using a Wax-based FuelHybrid Rocket Motor

Nozomu Kanno, Yuto Kanie (Meijo University), HiroumiTani, Yu Daimon (JAXA), Hiroshi Terashima (HokkaidoUniversity), Mitsuo Koshi (Yokohama NationalUniversity)

Ruwen Qu, Xiaoyu Wang, Xiaofeng Sun (BeihangUniversity)

Ryo Ando, Kazuki Kaneoya, Tetsuya Sato (WasedaUniversity), Hideyuki Taguchi, Hiroaki Kobayashi,Takayuki Kojima (JAXA)

Yoshikazu Sugiyama, Tomoya Suzuki, Kengo Chino,Kohei Kadohata, Hirokazu Tahara, Kyoko Takada(Osaka Institute of Technology)

Yuichi Nakada, Ichiro Nakagawa (Tokai University)

16:40～17:00 AJCPP2016-062 AJCPP2016-054 AJCPP2016-129 AJCPP2016-130 AJCPP2016-097Decomposition Mechanism of Propellants Based onHigh Energetic Materials

Instabilities inception in a single-stage transonic axialcompressor with circumferential groove

Mach 4 Wind Tunnel Firing Test of Hypersonic Pre-Cooled Turbojet

Experimental Investigations of High Power Quasi-Steady MPD Thruster

Numerical Analysis of Combustion Instability in Axial-Injected Hybrid Rocket Engines

Hiroki Matsunaga (Fukuoka University), Hiroto Habu(JAXA), Masaru Noda (Fukuoka University), AtsumiMiyake (Yokohama National University)

Byeung Jun Lim, Tae Choon Park, Young Seok Kang,Bong Jun Cha (KARI)

Takayuki Kojima, Hideyuki Taguchi, Hiroaki Kobayashi,Motoyuki Hongoh, Daisaku Masaki, Shunsuke Nishida,Sadatake Tomioka, Toshihito Saito, Shuichi Ueda,Kouichiro Tani (JAXA)

Yuya Oshio (JAXA), Satoshi Tonooka (The GraduateUniversity for Advanced Studies) Ikkoh Funaki (JAXA)

Goutham Karthikeyan, Toru Shimada (JAXA)

17:00～17:20 AJCPP2016-146 AJCPP2016-135 AJCPP2016-013 AJCPP2016-143 AJCPP2016-050Combustion and decomposition model of ammoniumdinitramide based propellant Isomerization ofdinitraminic acid (HDN)

Characteristics of Liquid Sheet Disintegration from theTrailing Edge of the Cascade Blade

CFD Study of Pseudo-Shock Waves in a RectangularDuct

A Development of power supply for AF 2D-MPD Change of Flow Structure in Shear Layer due to WallBlowing

Yu-ichiro Izato, Mitsuo Koshi, (Yokohama NationalUniversity), Hiroto Habu (JAXA), Atsumi Miyake(Yokohama National University)

Baber Javed, Toshinori Watanabe, Takehiro Himeno,Seiji Uzawa (The University of Tokyo)

Ruoyu Deng (Andong National University), ToshiakiSetoguchi (Saga University), Heuy Dong Kim (AndongNational University)

Shunichiro Ide (The University of Tokyo), RyodoTsukizaki, Hitoshi Kuninaka (JAXA)

Doyeong Kim, Young Joo Moon, Changjin Lee (KonkukUniversity)

17:20～17:40 AJCPP2016-072 AJCPP2016-147 AJCPP2016-133 AJCPP2016-119Prevention of Flashback in a Thruster with ADN-basedIonic Liquid Propellant

Effect of Inlet Distortion on AerodynamicCharacteristics of Axial Compressor Cascade

Combustion Characteristics for Small-scaledHypersonic Vehicle in Low Enthalpy Supersonic Flow

Flowfield Simulation for Development of High-PowerElectrothermal Pulsed Plasma Thrusters onboardOsaka Institute of Technology Second PROITERESNano-Satellite

Yuichiro Ide (The Graduate University for AdvancedStudies), Takuya Takahashi, Keiichiro Iwai, KatsuhikoNozoe (Carlit Holdings Co., Ltd.), Hiroto Habu,Shinichiro Tokudome (JAXA)

Kohei Horimoto, Toshinori Watanabe, Takehiro Himeno,Chihiro Inoue, Yasunori Sakuma (The University ofTokyo)

Chae-hyoung Kim, Yeoungmin Han (KARI), In-SeuckJeung (Seoul National University)

Masato Tanaka, Ryota Fujita, Keita Kanaoka, HirokazuTahara, Kyoko Takada (Osaka Institute of Technology)

17:40～18:00 AJCPP2016-152 AJCPP2016-153 AJCPP2016-121Numerical Analysis of Droplets Movement in AxialCompressor under Overspray Condition

Effects of Exhaust from Pre-Cooled Turbojet Engineon Ozone Concentration in Lower Stratosphere

Initial check out and EDVEGA phase operation ofHayabusa2 ion engine system

Atsushi Shimizu, Toshinori Watanabe, Takehiro Himeno,Chihiro Inoue (The University of Tokyo)

Yohei Asakami, Ichiyu Fujio, Shinji Nakaya, MitsuhiroTsue (The University of Tokyo)

Satoshi Hosoda, Kazutaka Nishiyama, Ryudo Tsukizaki,Hitoshi Kuninaka (JAXA)

Coffee break

March 18, 2016.

Room Room A Room B Room C Room D Room E

SessionChair

C0-chair

A-5:Jet Engine TechnologyYasunori Sakuma (The University of Tokyo)Youngbin Yoon (Seoul National University)

B-5:OS Thrusters -propellant, internal phenomenonand development-Yu Daimon (JAXA)

C-5:Scramjet and Ramjet 2Tetsuya Sato (Waseda University)

D-5:OS Electric propulsion: Hall thrusterNaoji Yamamoto (Kyushu University)

Satoshi Hosoda (JAXA)

E-5:Injector Technology in Rocket EnginesHee Jang Moon (Korea Aerospace University)

9:00～9:20 AJCPP2016-128 AJCPP2016-114 AJCPP2016-044Study on Upwash Generated by Impingement of TwoLiquid Sheets

Research and Development of Low-Power CylindricalHall Thrusters for Powered Flight onboard OsakaInstitute of Technology Nano-Satellite PROPITERES-3

Study on Flow Analysis of Hot Gas Valve with Pintle

Takao Inamura, Sosuke Endo, Koji Fumoto (HirosakiUniversity)

Tetsuo Kakuma, Taisuke Kagota, Yuya Takahata,Yusuke Furukubo, Mitsuyoshi Kobayashi, HirokazuTahara, Kyoko Takada (Osaka Institute of Technology),Tomoyuki Ikeda (Tokai University)

Kyungwook Lee (Hanbat National University), SeonukHeo, Sejin Kwon (KAIST), Jongkwang Lee (HanbatNational University)

9:20～9:40 AJCPP2016-011 AJCPP2016-061 AJCPP2016-028 AJCPP2016-118 AJCPP2016-048Effect of Rib Geometry in Turbulator Cooling onCooling Performance

Measurements of Spatial Distributions of Total MassFlux and Spray Mass Flux in Impinging Jet Atomization

Novel Vitiated Air Heater with Ethanol BlendedHydrogen Peroxide

Research and Development of High-Power, High-Specific-Impulse Hall Thruster for Manned MarsExploration

On the bubble breakup within an effervescent atomizer

Hidemi Toh, Syoma Furuta (Kanazawa Institute ofTechnology), Ryousuke Hinishi (IHI Jet Service)

Jun Hayashi, Daisuke Sato, Singo Karikawa (OsakaUniversity), , Yu Daimon, Hiroumi Tani (JAXA),Fumiteru Akamatsu (Osaka University)

W.S. Jung, S.K. Baek (KAIST), T.S. Kwon, J.H. Park(Defense R&D Institute), S.J. Kwon (KAIST)

Yuya Takahata, Taisuke Kagota, Tetsuo Kakuma,Yusuke Furukubo, Mitsuyoshi Kobayashi, HirokazuTahara, Kyoko Takada (Osaka Institute of Technology)

Moongeun Hong (KARI)

9:40～10:00 AJCPP2016-082 AJCPP2016-150 AJCPP2016-014 AJCPP2016-148 AJCPP2016-149Rough Weight Estimation for Intercooled andRecuperated Aviation Gas Turbine Using Airfoil HeatExchangers

Numerical Simulation of Impinging Jet Atomization forBi-propellant Thrusters

Supersonic Unsteady Cavity Flows Past Curved Walls Thrust measurement of high power RAIJIN Hallthruster using dual pendulum thrust stand

Effects of Total Momentum Ratio on CombustionBehavior in an Ethanol / Liquid Oxygen Rocket EngineCombustion Chamber with a Pintle Injector

Yutaka Ito (Tokyo Institute of Technology) Junya Kouwa, Shinsuke Matsuno (IHI), Yasuhito Kano(IHI Aerospace Co., Ltd) Atsushi Shimizu,Chihiro Inoue,Takehiro Himeno, Toshinori Watanabe (The Universityof Tokyo)

R. Das, A. R. Ye (Andong National University), T.Setoguchi (Saga University), H. D. Kim (AndongNational University)

Yushi Hamada, Yuya Hirano, Junhwi Bak, ReiKawashima, Tony Schoenherr, Kimiya Komurasaki,Hiroyuki Koizumi (The University of Tokyo)

Hiromitsu Kakudo, Kazuki Sakaki, Shinji Nakaya,Mitsuhiro Tsue (The University of Tokyo), KyoheiSuzuki, Ryuichiro Kanai, Takahiro Inagawa (InterstellerTechnologies), Tetsuo Hiraiwa (JAXA)

10:00～10:20 AJCPP2016-190 AJCPP2016-037 AJCPP2016-154 AJCPP2016-047 AJCPP2016-109Large Eddy Simulation of Collision Breakup andAtomization of a Liquid Jet into Cross Turbulent flows

Thruster Development in MHI (Mitsubishi HeavyIndustries, Ltd.)

Effect of Fuel Penetration Height on CombustionBehavior of Ethanol in a Scramjet Model Combustor

Hall Thruster Development for All-electric PropulsionSatellite and Deep Space Explorers

GCH4-Air Flame Characteristics of a Pintle InjectorDesigned for Liquid Rocket Engines in AtmosphericCondition

Young-lin Yoo, Hong-Gye Sung (Korea AerospaceUniversity)

Tetsuya Matsuo, Nobuhiko Tanaka, Hiroyuki Mishima,Katsumi Furukawa, Daijiro Shiraiwa, (MHI)

Yusuke Kawasumi, Naoki Igarashi, Shinji Nakaya,Mitsuhiro Tsue (The University of Tokyo), YasushigeUjiie (Nihon University)

Ikkoh Funaki (JAXA), Shigeyasu Iihara (IA), ShinatoraCho, Kenichi Kubota (JAXA), Watanabe Hiroki (TMU),Kenji Fuchigami, Yosuke Tashiro (IHI)

Min Son, Kijeong Yu, Kanmaniraja Radhakrishnan, JayeKoo (Korea Aerospace University)

Cancel10:20～10:40

SessionChair

C0-chair

A-6:Rocket Engine Technology 1Yutaka Ito (Tokyo Institute of Technology)

B-6:Fluid Dynamics 2Akiko Matsuo (Keio University)

Kuisoon Kim (Pusan National University)

C-6:Hypersonic Transport Propulsion 2Shinji Nakaya (The University of Tokyo)

D-6:OS Electric propulsion: Hall thrusterSatoshi Hosoda (JAXA)

Naoji Yamamoto (Kyushu University)

E-6:Hybrid Rocket 2Moongeun Hong (KARI)

10:40～11:00 AJCPP2016-139 AJCPP2016-070 AJCPP2016-145 AJCPP2016-086 AJCPP2016-021Design and performance comparison of centrifugal andmixed flow compressors with large flow coefficient

Study of the Velocity Profile in Turbulent BoundaryLayer over Flat Plate using PIV Measuremants atMach 3

Design of a Hypersonic Inlet without Concentration ofStrong Oblique Shock Waves

Effect of Magnetic Field Configuration on ThrustEfficiency in Anode layer type Hall Thrusters

Experimental Investigation of Gas NitrousOxide/Paraffin Hybrid Gas Generator for DuctedRocket

Yonghong Tang, Zhiheng Wang, Huijing Zhao, Guang Xi(Xi'an JiaoTong University)

Hyuk Lee, Young Ju Kim, Yung Hwan Byun, Soo HyungPark (Konkuk University)

Hideki Sawada, Tetsuya Sato (Waseda University) Yusuke Egawa, Naoji Yamamoto, Kohei Takase,Tomohiro Ichimaru, Hirotaka Fuchigami, Taichi Morita,Hideki Nakashima (Kyushu University)

Sunghoon Ryu, Seongjoo Han, Kyehwan Kim, JinkonKim , Heejang Moon (Korea Aerospace University),Junhyung Kim, Seung Won Ko (Agency for DefenseDevelopment)

11:00～11:20 AJCPP2016-140 AJCPP2016-071 AJCPP2016-015 AJCPP2016-172 AJCPP2016-046Effect of impeller trailing tip clearance flow on thevaned diffuser stall and the casing treatment

Study of the Velocity Profile in Transition BoundaryLayer over Flat Plate using Particle Image Velocimetryat M=3

Study on Unsteady Rayleigh Flows Magnetic Shielded Annular Hall Thruster with MagneticCircuits

Development of Hybrid Rocket Motor Design andPerformance Code

Tang Yonghong, Wang Zhiheng, Zhao Huijing, Xi Guang(Xi'an Jiaotong University)

Young Ju Kim, Hyuk Lee, Yung Hwan Byun, Soo HyungPark (Konkuk University)

Rajarshi Das, Lee IkIn, Vignesh Ram (Andong NationalUniversity), Toshiaki Setoguchi (Saga University),Heuy-Dong Kim (Andong National University)

Seunghun Lee, Holak Kim, Youbong Lim, Wonho Choe(KAIST)

Nazmi Erdi Coskunpinar, Kaan Ozen, Stanislav Grate,Alim Rustem Aslan (Istanbul Technical University)

Coffee Break

Room Room A Room B Room C Room D Room E11:20～11:40 AJCPP2016-185 AJCPP2016-094 AJCPP2016-023 AJCPP2016-029 AJCPP2016-079

Research on blade shape optmization of centrifugalimpeller using adjiont method

Effect of base bleed on the drag reduction of projectilein supersonic flow

Pressure Modeling in Turbulent SupersonicCombustion

PV Parameters Estimation Using a Developed IterativeMethod

Regression rate of a Swirling-injection End-BurningHybrid Rocket Engine using Paraffin-based Fuels

Jia Yu, Lucheng Ji (Beijing Institute of Technology),Hongying Ke, ,Weiwei LI, Weilin YI (Chinese Society ofEngineering Thermophysics),

Man Chul Jeong, Ji Hyun Park, In-Seuck Jeung (SeoulNational University), Hyoung Jin Lee (LIG Nex1)

Foluso Ladeinde (State University of New York Korea),Zhipeng Lou (Stony Brook University)

Tarek M. El-Sayed, Abd El-Shafy A. Nafeh, Faten H.Fahmy (Electronics Research Institute), Hosam K.M.Yousef (Cairo University)

Yuya Oishige, Daiki Hayashi, Takashi Sakurai (TokyoMetropolitan University)

11:40～12:00 AJCPP2016-040 AJCPP2016-103 AJCPP2016-095

An Experimental Setup for Analysis and Validation ofMaterials for Thermal Protection Systems usingPlasma Wind Tunnel

IDDES of a Hydrogen Combustion in a Model ScramjetCombustor using High-Order Spatial Discretization

Feasibility Study of Pre-Burner Lox Vaporization forSwirl Injection Hybrid Rocket Engine

Rajesh Kumar Chinnaraj, Gyusang Park, Sunmi Kim,Hana Jo, Philyong Oh, Seongman Choi (ChonbukNational University)

Junsu Shin, Hong-Gye Sung (Korea AerospaceUniversity)

Genki Mishima, Koki Kitagawa, Toru Shimada (JAXA)

12:00～13:00

SessionChair

C0-chair

A-7:OS More Electric Engine and Electric Propulsionfor Aircraft

Naoki Seki (IHI)

B-7:Non-Chemical Propulsion 2Kimiya Komurasaki (The University of Tokyo)

C-7: Combustion Technology 1Mitsumasa Makida（JAXA）

D-7:Rocket Engine Technology 2Takeshi Kanda (JAXA)

E-7:Jet Engine Technology 2Takehiro Himeno (The University of Tokyo)

13:00～13:20 AJCPP2016-031 AJCPP2016-116 AJCPP2016-035 AJCPP2016-188 AJCPP2016-158Development of Electric Propulsion System for a HighAltitude Solar UAV

Performance and Thermal Characteristics of Low-Power DC Arcjet Thrusters with Radiation-CooledAnodes for Low-Toxicity Propellants

Investigation of One Dimentional Nozzle DampingCharacterisitcs for Combustion Instability Supression

Effect of Multi-row vaned Diffusers on thePerformance of A Centrifugal Compressor Stage

Study on Variable Cycle Aero-engine Operation underthe Flight Condition

Keun-Bae Kim, Poomin Park, Bohwa Lee (KoreaAerospace Research Institute)

Suguru Shiraki, Yuki Fukutome, Fumihiro Inoue,Katsuya Shimogaito, Takashi Nakanishi, HirokazuTahara, Kyoko Takada (Osaka Institute of Technology),Yuichiro Nogawa (Splije)

Seunghyun Ryoo, Junseong Kim, Seongmin Joo,Hakchul Kim ,Honggye Sung, Heejang Moon (KoreaAerospace University), Dohyung Lee (Agency forDefense Development)

Yanjie Zhao, Feilong Dang, Jin Xiong, Jingyin Li ( Xi'anJiaotong University,

Asahi Owan, Naoki Akiyama (Tokyo University ofAgriculture and Technology), Yoshitaka Fukuyama,Takashi Yamane (JAXA)

13:20～13:40 AJCPP2016-032 AJCPP2016-164 AJCPP2016-059 AJCPP2016-090 AJCPP2016-041Flight Test of High Altitude Solar UAV’s ElectricPropulsion System

Development of 1A-class Microwave DischargeCathode

Simultaneous Optical Ignition and Spectroscopy of aTwo-Phase Spray Flame for Feedback Control

Analytical Study of Drive Mechanism for Multi-AxisPintle Thrusters

Engine Cycle Analysis of the Combined Tip JetRotorcraft

P. M. Park, B. H. Lee, K. B. Kim (Korea AerospaceResearch Institute)

Yoshitaka Tani (The University of Tokyo), RyudoTsukizaki (JAXA), Daiki Koda (The University ofTokyo), Kazutaka Nishiyama, Hitoshi Kuninaka (JAXA)

Seok Hwan Lee (Korea Research Institute ofStandards and Science), HyunWoo Kim, Hyungrok Do,Jack J. Yoh (Seoul National University)

Jaecheong Lee, Hwanil Huh. Hosung Lee(ChungnamNational University)

HaNa JO, SunMi Kim, Seong Man Choi (ChonbukNational University), Hyemin Kim, Gyaebyung Yang(Agency for Defense Development)

13:40～14:00 AJCPP2016-064 AJCPP2016-168 AJCPP2016-096 AJCPP2016-136 AJCPP2016-039Potential of SOFC-Hybrid Propulsion for ElectricAircraft

Measurements of the Ion Beam Accelerated from aNegative Ion Thruster Using Fullerene Propellant

An Investigation into the Combustion Characteristicsof Hydrocarbon Liquid-fuel Spray Generated byUltrasonic Atomization

A Visualization of the Gas-Liquid Swirl Coaxial-Injector Spray by Schlieren Photography

An Experimental Study of the Infrared SignalMeasurement using a Micro Turbo Jet Engine

Keiichi Okai, Atsushi Tateishi, Yasunori Sakuma,Takehiro Himeno, Toshinori Watanabe, TomohiroYokozeki (The University of Tokyo), Hiroshi Nomura(Nihon University), Takeshi Tagashira, Akira Nishizawa(JAXA)

Daiki Koda (The University of Tokyo), Hitoshi Kuninaka(JAXA)

Min Sung Kim, Seong Hun Bae, Jeong Soo Kim(Pukyong National University), Hyuk Soo Jeon, ChulHyon Park (Agency for Defense Development)

SeongHun Bae, MinSung Kim, JeongSoo Kim (PukyongNational University), HyuckSoo Jeon, ChulHyun Park(Agency for Defense Development)

Gyusang Park, Sunmi Kim, Seongman Choi (ChonbukNational University), Woncheol Kim (Agency forDefense Development)

14:00～14:20 AJCPP2016-106 AJCPP2016-183Fabrication of Lab-scale Tubular Solid Oxide Fuel Cellfor Basic Research on Fuel Cell - Gas TurbineCombined Electric Generator for Airplane

Temperature and Emittance Measurements ofKerosene Flame based on Radiation Spectroscopy

Daisuke Shimizu, Hiroshi Nomura, Yusuke Suganuma(Nihon University), Keiichi Okai (The University ofTokyo), Takeshi Tagashira, Akira Nishizawa (JAXA)

Yang Bin, Gui Xinyang, Ping Li, He Yuan (University ofShanghai for Science and Technology), Li Fang (BeijingInstitute of Aerospace System Engineering), CaiXiaoshu (University of Shanghai for Science andTechnology)

14:20～14:40

Lunch time

Coffee break

Room Room A Room B Room C Room D Room E

SessionChair

C0-chair

A-8:OS More Electric Engine and Electric Propulsionfor Aircraft

Keiichi Okai (The University of Tokyo)

B-8:Turbine TechnologyTakashi Yamane (JAXA)

C-8:Fluid Dynamics 3Seiji Tsutsumi (JAXA)

D-8: Combustion Technology 2Chihiro Inoue (The University of Tokyo)

E-8: Rocket EngineKazuyuki Yada (JAXA)

14:40～15:00 AJCPP2016-126 AJCPP2016-081 AJCPP2016-162 AJCPP2016-093 AJCPP2016-068Development and Flight Demonstration ofRegenerative Electric Propulsion System for AircraftApplication

Turbine Performance driven by a Pulse DetonationCombustor for Micro Gas Turbines

Numerical Simulation of Boundary LayerRelaminarizaion in Supersonic Expansion Flow

A Numerical Investigation of the Thermal Flow in anAxisymmetric Catalytic Combustor with DetailedSurface Chemistry

Extended Tsiolkovskii Equation and its Application toStudy on TSTO with RBCC

Akira Nishizawa, Hiroshi Kobayashi (JAXA), HiroshiFujimoto (The University of Tokyo)

Takashi Sakurai, Hiroto Takahashi, Yuki Hirai (TokyoMetropolitan University)

Hiroki Sanada, Susumu Teramoto, Koji Okamoto (TheUniversity of Tokyo)

Kumaresh Selvakumar, Man Young Kim (ChonbukNational University)

Takeshi Kanda, Kouchiro Tani, Kouichi Takasaki(JAXA)

15:00～15:20 AJCPP2016-167 AJCPP2016-159 AJCPP2016-049 AJCPP2016-104 AJCPP2016-123Development of Motor-Driven Fuel System for MoreElectric Engine

Influence of Radial locations of Inlet Hot Streak onAero-Thermal Performance of a 1-1/2 Stage GasTurbine

Numerical Analysis on Thrust Performance ofTruncated External Nozzle

Large Eddy Simulation of Supercritical Combustion ofOxygen and Kerosene of Coaxial Shear Injector

Integrated Mission, Sizing, and Design Process for LEORockets Development

Naoki Seki (IHI) Chen Zhang, Zhiduo Wang, Zhaofang Liu, ZhenpingFeng (Xi'an Jiaotong University)

Ryo Mikoshiba, Akiko Matsuo (Keio University),Tatsushi Isono (Tohoku University), Sadatake Tomioka(JAXA)

J. S. Kang, H.G. Sung (Korea Aerospace University), Jin-Wook Kim, Jae-Woo Lee, Sangho Kim (KonkukUniversity)

15:20～15:40 AJCPP2016-077 AJCPP2016-084 AJCPP2016-163 AJCPP2016-125Numerical Investigation of Nozzle Clocking Effect in 2-Stage Axial Flow Turbine

Influence of splitter blades of turbo on flow characterof bladeless fan

Effects of Atomization on Emissions in Reverse FlowFlame Stabilized Combustion

Study of Methane Fuel Rocket Engine Cycles

Ryuta Tanaka, Hiroshi Hamazaki, Masaaki Hamabe,Mizuho Aotsuka, Ruriko Yamawaki (IHI)

Hongya Mao, Peifeng Lin, Zhe Lin, Yanping Wang,Yingzi Jin (Zhejiang Sci-Tech University), ToshiakSetoguch (Saga University), Heuy Dong Kim (AndongNational University)

Takumi Hiroi, Takumi Saitou, Takafumi Nakasu, (HoseiUniversity), Hideshi Yamada (JAXA), Shigeru Hayashi(Hosei University)

Takeshi Kanda, Masaki Sato, Toshiya Kimura, HiroyaAsakawa (JAXA)

15:40～16:00 AJCPP2016-181 AJCPP2016-080Effects of Inlet Rotating Flow on Leading Edge FilmCooling in Double-passage Turbine Linear Cascades

Design and Sizing of Microwave Rocket Proposed forFirst Stage Rocket of Conventional Chemical Rocket

Yang Zhang, Yifei Li, Xin Yuan (Tsinghua University) Masafumi Fukunari, Kimiya Komurasaki, YusukeNakamura, Hiroyuki Koizumi (The University of Tokyo)

16:00～16:20

16:20～17:00

17:00～17:40

17:40～18:20

18:20～19:00

19:00～21：00

Propulsion Systems For Korean Lunar Exploration Proguram

Prof. Yung hwan Byun (Konhuk University)

AJCPP2016-S02

Climbing up the global sky, Kawasaki innovative Technologies

Mr. Yasuhiro Kinoshita(KHI)

AJCPP2016-S03

Break

Room A L-2:Keynote Speech　　Prof. Mitsuhiro Tsue (The University of Tokyo)

AJCPP2016-S04

Flow control technique in compressor and turbine

Prof. Bo Liu (Northwestern Polytechnic University)

Banquet (Hiten, JR Hotel Clement Takamatsu)

Break

Extraction of detailed reaction kinetics of aluminized RDX using isoconversional method and isothermal DSC for propulsion

Yoocheon Kim and Jack J. Yoh

Department of Mechanical and Aerospace Engineering, Seoul National University Gwanak-ro 1, Gwanak-gu, Seoul, Korea, 151-742

jjyoh@snu.ac.kr

Kuktae Kwon and Jungsu Park

4th R&D Institute-2, Agency for Defense Development Daejeon, Korea, 305-600

Keywords: Propulsion, Reaction Kinetics, Aluminized RDX,

Isoconversional Method, DSC, Numerical Simulation

Abstract

The kinetic analysis of a heavily aluminized

cyclotrimethylene-trinitramine (RDX) using Isoconversional method and Differential Scanning Calorimetry (DSC) is conducted. The Friedman isoconversional method is applied to DSC experimental data. To resolve the phase transition problem occurred prior to exothermic chemical reaction during non-isothermal DSC experiment, set of isothermal DSC experiments are conducted.

In the present work, the pre-exponential factor and activation energy are extracted as a function of product mass fraction. The extracted kinetic scheme does not assume multiple chemical steps to describe the complex response of energetic materials; instead, a set of multiple Arrhenius factors is constructed based on the local progress of the exothermic reaction.

The resulting reaction kinetic scheme is applied to two thermal decomposition tests and a shock-initiation test for validating the reactive flow response of a heavily aluminized RDX. Present kinetic scheme shows good reproducibility of practical thermal test. And it has advantage about numerical accuracy and efficiency compared to conventional reaction kinetics such as one-step or multi-step kinetics.

Introduction

The understanding of the behavior of energetic materials is of broad interest to the energetic materials community for the purposes of safe handling, suitable storage methods, and comprehension of reaction violence. In particular, accurate kinetics is essential for predicting the reactive flow behavior of energetic materials.

Several approaches to the determination of the reaction profiles of energetic materials have been proposed. The first one develops a detailed mechanism that covers more than a hundred reactions [1]. Most of such high energy materials have complex reaction paths which cannot be described by a single reaction step. Nevertheless, kinetics composed of too many specific reactions is not suitable for efficient computational chemistry for its exhaustively

demanding computing time. The second one, a multi-step scheme, assumes only a few reaction steps which have dominance on the global chemical reaction [2, 3]. With the third approach, based on the Coats-Redfern method [4], the scheme is similar to a global scheme of the multi-step approach but it uses only a single reaction step. With this approach, as the reaction progresses a limited set of parameters are assigned per certain degree of conversion, resulting in relatively poor accuracy while calculation time is significantly improved. The last approach is an enhancement to the isoconversional method of Friedman [5]. The method addresses activation energy and the pre-exponential factor which varies with each degree of conversion during the entire reaction. This has gained much attention thanks to noticeable progress in the integral method [6] and in the availability in the form of kinetics analysis software [7]. The kinetics obtained in this way does not assume multiple chemical steps; instead, a set of multiple Arrhenius factors is constructed based on the local progress of the exothermic reaction. For this reason, we focus on the last approach for building the reaction kinetics for reactive flow response of the desired energetic materials.

To obtain the kinetics of reactive materials based on thermal stimulus, several types of thermal tests such as thermogravimetric analysis (TGA), scaled thermal explosion (STEX), one-dimensional time to explosion (ODTX) and differential scanning calorimetry (DSC) have been in use. Each of these experiments has its distinct scales and amounts of target samples required for reliable data acquisition.

In this paper, DSC experiments are conducted to extract the kinetics of a multi-purpose energetic material which is comprised of 50% RDX (cyclotrimethylene-trinitramine) and 35% aluminum powder with 15% HTPB (hydroxyl-terminated polybutadiene) binder, and its initial density after pressing is 1.78 g/cc. The DSC has been mainly used to measure the thermal decomposition characteristics of energetic materials [7,8]. The kinetic scheme derived using DSC and the isoconversional method is essentially a single step with a multiple set of Arrhenius parameters that time-evolve with the