櫻井 毅司（サクライ タカシ） 2015年度

研究業績

学会発表（国内）

1. 高橋瞬、櫻井毅司：ハイブリッドロケットエンジン用燃料グレインのメタン/酸素火炎による着火、第53回燃焼シンポジウム、C212、2015, pp.242-243．

学会発表（国際）

1. Tomizawa, T., Sakurai, T.: Applicability of a LOx Vaporization Preburner for Swirling- -Flow Hybrid Rocket Engines, 51st AIAA Joint Propulsion Conference, AIAA 2015-4134, 2015.
2. Hayashi, D., Sakurai, T.: A Fundamental Study of An End-Burning Swirling-Flow Hybrid Rocket Engine Using Low Melting Temperature Fuels, 51st AIAA Joint Propulsion Conference, AIAA 2015-4138, 2015.
3. Sakurai, T., Yuasa, S., Ando, H., Kitagawa, K., Shimada, T.: Fuel Regression Rate Characteristics of the Swirling-Oxidizer-Flow-Type Hybrid Rocket Engine, 12th ICFD, OS8-2, 2015, pp.382-383.
4. Harada, R., Kobori, Y., Sakurai, T.: Development of a Prevaporized Combustor using a Porous Media for a Kerosene-fueled Micro Gas Turbine, Proc. International Gas Turbine Congress 2015, MoAMA.1, 2015.
5. Takahashi, H., Hirai, Y., Sakurai, T.: Fundamental Study of a Micro Gas Turbine with a Detonation Combustor, Proc. International Gas Turbine Congress 2015, MoAMA.2, 2015.
6. Oishige, Y., Hayashi, D., Sakurai, T.: Regression rate of a Swirling-injection End-Burning Hybrid Rocket Engine using Paraffin-based Fuels, Proc. Asian Joint Conference on Propulsion and Power, AJCPP2016-079, 2016.
7. Sakurai, T., Takahashi, H., Hirai, Y.: Turbine Performance driven by a Pulse Detonation Combustor for Micro Gas Turbines, Proc. Asian Joint Conference on Propulsion and Power, AJCPP2016-081, 2016.

国内の他機関との連携による研究活動実績

1. JAXA/ISASハイブリッドロケットWG委員