Proj
J-GLOBAL ID:200904095736811405  Research Project code:0250002654 Update date:Feb. 12, 2003

Fluid-dynamic experiment on atmosphere re-entry in super-orbit-velocity

超軌道速度大気圏再突入に関する流体力学実験
Study period:2000 - 2000
Research overview:
This study examined the generation method of testing conditions of the fluid-dynamic simulation experiment of the super-orbit-velocity atmosphere re-entry using the expansion tube. The values as the stagnation point enthalpy of 37MJ/kg and the testing time of 12 mu s. The obtained results on the forms of shock waves and the distance of shock wave isolation were consistent with the calculated values provided by Shizuoka University and Institute of Space and Aeronautic Science.
Research program: -
Ministry with control over the research :
Ministry of Education, Culture, Sports, Science and Technology

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