J-GLOBAL ID:200904070524311574  Research Project code:0250002665 Update date:Jan. 19, 2004

Study on impact properties of the reentrance capsule structure

Study period:2000 - 2002
Organization (1):
Investigating Researcher (4):
Research overview:
We estimate thermal stress and thermal deformation at the reentrance, load of static acceleration during aerodynamic speed reduction, load of impact of opening parachute, load of landing impact and machinery environment of loading equipment, and we also develop the lightweight structure which shall be sustainable to them.
Research program: Ordinary Research
Ministry with control over the research :
Ministry of Education, Culture, Sports, Science and Technology

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