1. Combustion, Thermal Engineering
2. Propultion/Engine, Aerospace Engineering

1. Intrinsic instability of premixed flame
2. Flame acceleration characteristics of hydrogen flame
3. Combsution characteristics of ionic liquid propellnat
4. Laser ignition

1. Vacuum chamber for thruster firing test
2. Laser measurement system
3. Laser ignition system
4. Schlieren system
5. Closed chamber for gas explosion test

1. Measurement and observation of flame
2. Experiment of gas combustion
3. Combustion experiment of high energetic materials
4. Research and development of space propulsion system
5. Risk assesment for combustion equipments

1. High performance gas generator
2. Hydroxylammonium nitrate based propellnat for thruster
3. Catalytic thruster for ionic liquid propellant

1. Combustion mesurement and control
2. Combustion safety
3. Renewable energy
4. Space propulsion system

1. No. JP,5721371,B
2. No. JP,5250873,B
3. No. JP,5326158,B
4. No. JP,5376132,B
5. Gas generating composition, No. US8114228 B2
6. No. JP,5110256,B