応用科学群 応用化学科 火薬学 准教授 甲賀 誠 本文へジャンプ
学術論文

1990-1999
2000-2009

2010-2019
2020-

1990-1999

 1 萩原 豊,市川敏夫,鈴木正大,甲賀 誠
AP/HTPB系コンポジット推進薬の燃焼速度におよぼす各種酸化鉄の効果(I)
工業火薬
,第52巻,第6号,pp.396~399 (1991.12)
 2 萩原 豊,市川敏夫,鈴木正大,甲賀 誠
AP/HTPB系コンポジット推進薬の燃焼速度におよぼす各種酸化鉄の効果(II)―粉砕の効果―
工業火薬
,第53巻,第3号,pp.125~130 (1992.6)
 3 甲賀 誠,鈴木正大,萩原 豊
AP/HTPB系推進薬の燃焼速度に及ぼす各種水酸化第2鉄の効果
工業火薬
,第53巻,第6号,pp.285~290 (1992.12)
 4 甲賀 誠,鈴木正大,萩原 豊
凍結乾燥法で調製した微粒過塩素酸アンモニウム―針状過安を用いた場合
工業火薬
,第53巻,第6号,pp.295~300 (1992.12)
 5 甲賀 誠,鈴木正大,萩原 豊
凍結乾燥法で調製した微粒過塩素酸アンモニウムを用いた推進薬(第3報)―針状過安を用いた場合
工業火薬
,第54巻,第2号,pp.64~69 (1993.4)
 6 甲賀 誠,萩原 豊
噴霧乾燥法による微粒な多孔質過塩素酸アンモニウムの調製
粉体工学会誌
,第33巻,第4号,pp.273~278 (1996.4)
 7 甲賀 誠,萩原 豊
凍結乾燥法による微粒過塩素酸アンモニウムの調製
化学工学論文集
,第23巻,第2号,pp.163~169 (1997.3)
 8 荒川洋一,甲賀 誠,都筑寛達,萩原 豊
硝酸アンモニウム系推進薬の燃焼特性―硝酸アンモニウムの平均粒径の影響
火薬学会誌
,第58巻,第2号,pp.76~82 (1997.4)
 9 荒川洋一,甲賀 誠,都筑寛達,萩原 豊
硝酸アンモニウム系推進薬(第2報)―未硬化推進薬の粘性に及ぼす界面活性剤の添加効果
火薬学会誌
,第58巻,第2号,pp.83~88 (1997.4)
 10 甲賀 誠,萩原 豊
噴霧乾燥法による微粒過塩素酸アンモニウムの調製―粒子の形状と粒径に及ぼす有機溶剤の効果
粉体工学会誌
,第34巻,第6号,pp.437~442 (1997.6)
 11 甲賀 誠,萩原 豊
超音波微粒化法を用いた過塩素酸アンモニウムの噴霧乾燥
粉体工学会誌
,第34巻,第7号,pp.522~527 (1997.7)
 12 萩原 豊,甲賀 誠,鈴木正大,都筑寛達,荒川洋一
晶癖変化している過塩素酸アンモニウム(第1報)―粒子ならびに熱分解特性について
火薬学会誌
,第58巻,第6号,pp.237~244 (1997.12)
 13 M. Kohga,Y. Hagihara
Experimental Study on Processability of Ammonium Perchlorate/Hydroxyl-terminated Polybutadiene Composite Propellant(Ⅰ)-Influences of Operating Temperature on Viscosity of Uncured Propellant
J. Japan Explosives Soc.,Vol.59,No.1,pp.1~5 (1998.2)
 14 甲賀 誠,萩原 豊
過塩素酸アンモニウム/末端水酸基ポリブタジエン分散系の流動特性による最大容積濃度の評価
粉体工学会誌
,第35巻,第7号,pp.482~490 (1998.7)
 15 M. Kohga,Y. Hagihara
Experimental Study on Estimation of Upper Limit of Ammonium Perchlorate Content in Ammonium
Perchlorate/Hydroxyl-terminated Polybutadiene Composite Propellant
Transactions of the Japan Society for Aeronautical and Space Sciences,Vol.41,No.132,pp.74~78 (1998.8)
 16 M. Kohga,Y. Hagihara
Effects of Addition of Surfactants on Viscosity of Uncured Ammonium Perchlorate/Hydroxyl-terminated Polybutadiene Propellant
J. Japan Explosives Soc.,Vol.59,No.4,pp.167~173 (1998.8)
 17 M. Kohga,Y. Hagihara
Burning Behavior of Composite Propellant Containing Fine Porous Ammonium Perchlorate
Propellants, Explosives, Pyrotechnics,Vol.23,No.4,pp.182~187 (1998.8)
 18 萩原 豊,甲賀 誠,鈴木正大,寺田秀一
晶癖変化している過塩素酸アンモニウム(第2報)―それらを用いた推進薬の製造性ならびに燃焼特性
火薬学会誌,第60巻,第6号
,pp.279~285 (1999.12)
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2000-2009
19  M. Kohga,Y. Hagihara
AP/HTPB Composite Propellant Using Fine AP Prepared by Freeze-drying Method(IV) -Fine AP Prepared from Emulsion with Toluene and AP Solution-
J. Japan Explosives Soc.,Vol.61,No.2,pp.51~57 (2000.4)
 20 M. Kohga,Y. Hagihara
Estimation of Upper Limit of AP Content in AP/HTPB Composite Propellant -A Consideration Based on Flow Characteristics of AP/HTPB Suspension
J. Japan Explosives Soc.,Vol.61,No.4,pp.157~166 (2000.8)
 21 M. Kohga,Y. Hagihara
Rheology of Concentrated AP/HTPB Suspension Prepared at Upper Limit of AP Content
Propellants, Explosives, Pyrotechnics,Vol.25,No.4,pp.199~202 (2000.8)
 22 甲賀 誠,萩原 豊
多成分系化による過塩素酸アンモニウムの最粗充填における空隙率の低下
火薬学会誌
,第61巻,第5号,pp.216~223 (2000.10)
 23 寺田秀一甲賀 誠,萩原 豊
高分子でコーティングされた
ANを用いたAN系コンポジット推進薬の燃焼特性
Science and Technology of Energetic Materials,Vol.64,No.1,pp.9~15 (2003.2)
 24 M. Kohga,Y. Hagihara
Self-quenched Combustion of Fuel-rich AP/HTPB Composite Propellant
Science and Technology of Energetic Materials,Vol.64,No.2,pp.68~74 (2003.4)
 25 M. Kohga,Y. Hagihara
AP/HTPB Composite Propellant Using Fine Hollow AP Prepared by Spray-drying Method
Science and Technology of Energetic Materials,Vol.64,No.2,pp.75~80 (2003.4)
 26 M. Kohga,Y. Hagihara
Burning Characteristics of Fuel-rich AP/HTPB Composite Propellant Added with Iron Oxide
Science and Technology of Energetic Materials,Vol.64,No.3,pp.110~115 (2003.6)
 27 M. Kohga,Y. Hagihara
Estimation of Highest Burning Rate of AP/HTPB Composite Propellant with Experimental Approach(I) -Burning Rate Characteristics of AP/HTPB Composite Propellant-
Science and Technology of Energetic Materials,Vol.64,No.4,pp.153~160 (2003.8)
 28 M. Kohga,Y. Hagihara
Estimation of Highest Burning Rate of AP/HTPB Composite Propellant with Experimental Approach(Ⅱ) -Estimation of Highest Burning Rate by Use of AP Particle Property-
Science and Technology of Energetic Materials,Vol.64,No.4,pp.161~166 (2003.8)
 29 M. Kohga,Robert A. Frederick Jr., Marlow D. Moser
Ultrasonic Properties of Propellant Ingredients
Journal of Propulsion and Power,Vol.20,No.1,pp.135~140 (2004.2)
 30 M. Kohga
Burning Characteristics of AP/HTPB Composite Propellants Prepared with Fine Porous or Fine Hollow AP
Propellants, Explosives, Pyrotechnics,Vol.31,No.1,pp.50~55 (2006.2)
 31 吉田冴子,甲賀 誠
微粒
APと粗粒APを用いたAN/AP系推進薬の燃焼特性
Science and Technology of Energetic Materials,Vol.67,No.4,pp.117~123 (2006.8)
 32 M. Kohga,W. Miyano,T. Kojima
Burning Characteristics of Polytetrahydrofuran-based Composite Propellant
Journal of Propulsion and Power,Vol.22,No.6,pp.1418~1421 (2006.12)
 33 甲賀 誠
AP/HTPB
系コンポジット推進薬設計のための一考察
日本航空宇宙学会論文誌
,Vol.55,No.4,pp.182~187 (2007.4)
 34 K. Iwakuma, Y. Miyata, S. Date, M. Kohga, K. Hasue
A Study on the Combustion of 5,5’-Azobis-Tetrazole Aminoguanidine/Strontium Nitrate as a Gas Generating Agent
Science and Technology of Energetic Materials,Vol.68,No.4,pp.95~101 (2007.8)
 35 M. Kohga
Burning Rate Characteristics of AP-Based Composite Propellant Using Bimodal AP
Journal of Propulsion and Power,Vol.24,No.3,pp.499~506 (2008.5)
 36 M. Kohga
Effect of Voids inside AP Particles on Burning Rate of AP/HTPB Composite Propellant
Propellants, Explosives, Pyrotechnics,Vol.33,No.4,pp.249~254 (2008.8)
 37 Y. Miyata, M. Abe, S. Date, M. Kohga, K. Hasue
Burning Characteristics of Aminoguanidium 5,5'-azobis-1H-tetrazole/Ammonium Nitrate as Gas Generating Mixtures
Science and Technology of Energetic Materials,Vol.69,No.4,pp.117~122 (2008.8)
 38 M. Kohga, S. Yoshida, K. Hasue
Influence of AP Particle Size on the Bunring Characteritics of AN/AP-Based Composite Propellants
International Journal of Energetic Materials and Chemical Propulsion, Vol.7, No.6, pp.491~506 (2008.9)
 39 M. Abe, T. Ogura, Y. Miyata, K. Okamoto, S. Date, M. Kohga, K. Hasue
Evaluation of Gas Generating Ability of Some Tetrazoles and Copper(II) Oxide Mixtures Through Closed Vessel Test and Theoretical Calculation
Science and Technology of Energetic Materials,Vol.69,No.6,pp.183~190 (2008.12)
 40 Y. Miyata, M. Abe, S. Date, M. Kohga, K. Hasue
The Kinetics of the Main Decomposition Process of Aminoguanidium 5,5-azobis-1H-tetrazolate
Propellants, Explosives, Pyrotechnics,Vol.34,No.2,pp.110~119 (2009.4)
 41 M. Kohga, K. Okamoto
Burning Characteristics and Mechanical Properties of AP/HTPB Propellant Containing Glycerin as a Plasticizer
Transactions of Japan Society for Aeronautical and Space Sciences, Space Technology Japan, Vol. 7, No.ists26, pp.Pa_53~Pa_57 (2009.8)
 42 M. Kohga, S. Nishino
Burning Characteristics of Ammonium Nitrate-based Composite Propellants Supplemented with Ammonium Dichromate
Propellants, Explosives, Pyrotechnics,Vol.34,No.4,pp.340~346 (2009.8)
43 岡本香預子,甲賀 誠,蓮江和夫
PTHF/HTPBブレンドの熱的挙動と引張り特性
Science and Technology of Energetic Materials,Vol.70,No.4,pp.87~93 (2009.8)
 44 M. Kohga, S. Nishino
From Crosslinking to Plasticization -Characterization of Glycerin/HTPB Blends
Propellants, Explosives, Pyrotechnics,Vol.34,No.5,pp.436~443 (2009.10)
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2010-2019
 45 M. Kohga, H. Tsuzuki
Crystal Habit Modification of Ammonium Perchlorate by Ethylene Glycol
Advanced Powder Technology, Vol.21, No.4, pp.443~447 (2010.7)
 46 M. Kohga
Application of Polytetrahydrofuran as a Plasticizer of HTPB Binder
Science and Technology of Energetic Materials, Vol.71, No.3, pp.77~82 (2010.8)
 47 甲賀 誠
可塑剤としてPolytetrahydrofuranを用いたAP/HTPB系推進薬の機械的特性と燃焼特性
Science and Technology of Energetic Materials, Vol.71, No.6, pp.145~150 (2010.12)
 48 M. Kohga, K. Okamoto
Burning Characteristics and Thermochemical Behaviour of AP/HTPB Composite Propellant Using Coarse and Fine AP Particles
Propellants, Explosives, Pyrotechnics,
Vol.36, No.1, pp.5764 (2011.2)
 49 M. Kohga
Thermal Decomposition Behaviors and Burning Characteristics of Ammonium Nitrate/
Polytetrahydrofuran/Glycerin Composite Propellant
Combustion and Flame, Vol.158, No.3, pp.573~582 (2011.3)
 50 M. Kohga, H. Tsuzuki
Burning rate characteristics of Composite Propellant Using Ammonium Perchlorate Modified by Ethylene Glycol
Journal of Propulsion and Power, Vol.27, No.3, pp.668~674 (2011.5)
 51 M. Kohga
Viscoelastic Behavior of Hydroxyl Terminated Polybutadiene Containing Glycerin
Journal of Applied Polymer Science, Vol.122, No.1, pp.706~713 (2011.10)
52 M. Kohga, K. Okamoto
Thermal Decomposition Behaviors of AN-based Composite Propellant with Hydroxyl-terminated Polybutadiene/Polytetrahydrofuran Blend as a Binder
Science and Technology of Energetic Materials, Vol.72, No.6, pp.161168 (2011.12)
 53 M. Kohga, T. Naya, K. Okamoto
Burning Characteristics of Ammonium Nitrate-based Composite Propellants with a Hydroxyl-
Terminated Polybutadiene/Polytetrahydrofuran Blend Binder
International Journal of Aerospace Engineering, Vol.2012, Article ID 378483, pp.1~9 (2012.4)
 54 M. Kohga
Dynamic Mechanical Properties of Hydroxyl-terminated Polybutadiene Containing Polytetrahydrofuran as a Plasticizer
Nihon Rheology Gakkaishi, Vol.40, No.4, pp.185~193 (2012.9)
 55 T. Naya, M. Kohga
Burning Characteristics of Ammonium Nitrate-based Composite Propellants Supplemented with
MnO
2
Propellants, Explosives, Pyrotechnics, Vol.38, No.1, pp.87~94 (2013.2)
 56 M. Kohga, T. Naya, S. Shioya
Viscoelastic and Thermal Decomposition Behaviors of Polytetrahydrofuran Binder Prepared Using
Glycerin as a Crosslinking Modifier
Journal of Applied Polymer Science, Vol.128, No.3, pp.2089~2097 (2013.5)
 57 T. Naya, M. Kohga
Influences of Particle Size and Content of HMX on Burning Characteristics of HMX-based
Propellant
Aerospace Science and Technology, Vol.27, No.1, pp.209~215 (2013.6)
 58 M. Kohga
Mechanical Characteristics and Thermal Decomposition Behaviours of Polytetrahydrofuran Binder
Using Glycerol Propoxylate (Mn=260) as a Crosslinking Agent
Propellants, Explosives, Pyrotechnics, Vol.38, No.3, pp.366~371 (2013.6)
 59 T. Naya, M. Kohga
Burning Characteristics of Ammonium Nitrate-based Composite Propellants Supplemented with
Fe
2O3
Propellants, Explosives, Pyrotechnics, Vol.38, No.4, pp.547~554 (2013.8)
 60 S. Shioya, M. Kohga, T. Naya
Burning Characteristics of Ammonium Perchlorate-based Composite Propellant Supplemented with Diatomaceous Earth
Combustion and Flame, Vol.161, No.2, pp.620~630 (2014.2)
 61 T. Naya, M. Kohga
Influence of Fe2O3 Size on Burning Characteristics of Ammonium Nitrate/Fe2O3 Propellants
Journal of Propulsion and Power,
Vol.30, No.3, pp.864~866 (2014.5)
 62 T. Naya, M. Kohga
Thermal Decomposition Behaviors and Burning Characteristics of AN/Nitramine-based Composite
Propellant
Journal of Energetic Materials, Vol.33, No.2, pp.73~90 (2015.4)
 63 M. Kohga, T. Naya
Thermal Decomposition Behaviors and Burning Characteristics of AN/RDX-based Composite
Propellants Supplemented with MnO2 and Fe2O3
Journal of Energetic Materials, Vol.33, No.4, pp.288~304 (2015.8)
 64 M. Kohga, S. Handa
Preparation of Combined Ammonium Perchlorate/Ammonium Nitrate Samples by Freeze-drying
Journal of Energetic Materials, Vol.35, No.3, pp.276~291 (2017.6)
 65 M. Kohga
Thermal Decomposition Behaviors and Burning Characteristics of Ammonium Nitrate/ Polytetrahydrofuran/Glycerin-based Composite Propellants Supplemented with MnO
2 and Fe2O3
Propellants, Explosives, Pyrotechnics, Vol.42, No.6, pp.665~670 (2017.6)
 66 M. Kohga
Mechanical Characteristics and Thermal Decomposition Behaviors of Polytetrahydrofuran Binder
with Glycerol Propoxylate (M
n=1500) as a Crosslinking Agent
Propellants, Explosives, Pyrotechnics, Vol.42, No.11, pp.1283~1288 (2017.11)
 67 M. Kohga, S. Hande
Thermal Decomposition Behaviors and Burning Characteristics of Composite Propellants Prepared
Using Combined Ammonium Perchlorate/Ammonium Nitrate Particles
Journal of Energetic Materials,Vol.36, No.1, pp.93~110 (2018.1)
68 M. Kohga, S. Togo
Influence of Iron Oxide on Thermal Decomposition Behavior and Burning Characteristics of
Ammonium Nitrate/Ammonium Perchlorate-based Composite Propellants
Combustion and Flame,Vol.192, pp.10~24 (2018.6)
 69 M. Kohga, D. Shigi, M. Beppu
Detonation Properties of Ammonium Nitrate/Nitramine-based Composite Propellants
Journal of Energetic Materials,Vol.37, No.3, pp.309~319 (2019.7)
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2020-
 70 M. Kohga, S. Togo
Influence of MnO2 and Fe2O3 on the Burning Characteristics of AN/AP-based Composite
Propellants
Propellants, Explosives, Pyrotechnics, Vol.45, No.1, pp.141~146 (2020.1)
 71 M. Kohga, S. Togo
Catalytic Effect of Added Fe2O3 Amount on Thermal Decomposition Behaviors and Burning Characteristics of Ammonium Nitrate/Ammonium Perchlorate Propellants
Conbustion Science and Technology, Vol.192, No.9, pp.1668~1681 (2020.9)
 72 R. Togashi, M. Kohga
Preparation of Fine Ammonium Perchlorate by Employing Dual-sonic Premixer:
Freeze-drying Method

Propellants, Explosives, Pyrotechnics, Vol.46, No.6, pp.855~859 (2021.6)
 73 M. Kohga, R. Togashi
Mechanical Properties and Thermal Decomposition Behaviors of Hydroxyl-terminated
Polybutadiene/Glycerol Propoxylate Blend and its Application to Ammonium Nitrate-based
Propellants

Propellants, Explosives, Pyrotechnics, Vol.46, No.7, pp.1016~1022 (2021.7)
 74 N. Tsuchiya, M. Kohga
Preparation of Fine Porous Ammonium Perchlorate by Spray-drying Method and Evaluation of its
Performance as a Propellant Oxidizer
Memoirs of the National Defense Academy, Japan, Vol. 61, No. 2, pp. 1~9 (2022.3)
 75 M. Kohga, R. Togashi, N. Tsuchiya, Y. Ota
Catalytic Effect of Ferric Oxide on Burning Characteristics of Propellants Using Ammonium
Perchlorate with Varied Particle Properties
Combustion and Flame, Vol. 246, 112459 (2022. 12)
   

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