spacecraft thermal and fluids systems f …...2009.3.1 9 institute of fluid science, tohoku...
TRANSCRIPT
2009.3.1
9 1 Institute of Fluid Science, Tohoku University
Spacecraft Thermal and Fluids Systems Laboratory, Institute of Fluid Science
Nagai∙Fujita Lab.
Lab HP: http://www.ifs.tohoku.ac.jp/space/ E-mail: [email protected]
Study of aerodynamic characteristics and heating phenomena when a space vehicle enters into planet atmosphere
Development of thermal control device and innovative thermal system for next-generation spacecraft
Study and Development of Mars airplane / helicopter
Progressive visualization, measurement technique challenge under extreme environment
Aerodynamic heating of Hypersonic airplane
HIFiRE-1 model in JAXA-HIEST
Study of Mars airplane
Martian hole and lava tube exploration using rotorcraft
Thermal control of spacecraft (Understand and manage the heat)
Aerospike Model
Loop Heat Pipe Oscillating Heat Pipe
Aerodynamic heating (Database for spacecraft design)
Compression Corner Model
N
N
N
NM
FF
F
F
F
FF
F
F F
F
FF
F
F
F F
F
FF
N
N
N
NM
FF
F
F
F
FF
F
F F
F
FF
F
F
F F
F
FF
Re-entry Capsule
Micro-nozzle
Thermal / aerodynamic measurement in extreme conditions （High / low temperature, Reynolds number, Mach number, Knudsen number）
NN
NN
N
NRu
2+CH3
Si(CH3)3
n
Thermal Analysis of Mars Airplane
groove
ウィック前面 ウィック側面