観測ロケットを利用した燃料液滴冷炎燃焼実験の装置開発

抄録

As fundamental research on spray combustion, spontaneous ignition phenomenon is important and research has been conducted by various approaches. The Japan-German joint research program “PHOENIX-2” aims to clarify 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 underway.