Hardware Development for Cool Flame Combustion Experiment of Fuel Droplets using Sounding Rocket

被引：4

作者：

Suganuma, Yusuke ^{[1
]}

Saito, Masanori ^{[2
]}

Goto, Yoshimasa ^{[3
]}

Yamamura, Yoshiyuki ^{[3
]}

Yamamoto, Shin ^{[3
]}

Nokura, Masaki ^{[3
]}

Mikami, Masato ^{[4
]}

Kikuchi, Masao ^{[5
]}

Inatomi, Yuko ^{[6
]}

Moriue, Osamu ^{[7
]}

Nomura, Hiroshi ^{[1
]}

Tanabe, Mitsuaki ^{[2
]}

机构：

[1] Nihon Univ, Coll Ind Technol, 1-2-1 Izumi Cho, Narashino, Chiba 2758575, Japan

[2] Nihon Univ, Coll Sci & Technol, 7-24-1 Narashinodai, Funabashi, Chiba 2748501, Japan

[3] IHI Inspect & Instrumentat CO Ltd, 1-100 Takamatsu Cho, Tachikawa, Tokyo 1900011, Japan

[4] Yamaguchi Univ, Dept Mech Engn, 2-16-1 Tokiwadai, Ube, Yamaguchi 7558611, Japan

[5] Japan Aerosp Explorat Agcy, 2-1-1 Sengen, Tsukuba, Ibaraki 3058505, Japan

[6] Japan Aerosp Explorat Agcy, Chuo Ku, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 2525210, Japan

[7] Kyushu Univ, Fac Engn, Nishi Ku, 744 Motooka, Fukuoka 8190395, Japan

来源：

INTERNATIONAL JOURNAL OF MICROGRAVITY SCIENCE AND APPLICATION | 2020年 / 37卷 / 04期

关键词：

Cool flame; Droplet; Spontaneous ignition;

D O I：

10.15011/jasma.37.4.370403

中图分类号：

O59 [应用物理学];

学科分类号：

摘要：

As fundamental research on spray combustion, spontaneous ignition phenomenon is important and research has been conducted by various approaches. The Japan-Gennan joint research program "PLIOENIX-2" aims to ignition process accompanying the cool flame around ignition limit by utilizing a TEXUS sounding rocket and it is very important study conjunction with the vaporization and flame spread. The design of the experimental equipment has been carried out by confirming the functions of each part by conducting element prototypes and parabolic flight experiments. At present, the detailed design review has been completed and the production phase is is underway.

引用

页数：5

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