J-GLOBAL ID:201110069367762560   Research Resource code:5000002727 Update date:Dec. 15, 2003

MTS 500kN fatigue testing Machine

Owning Organization:
Contact: TERADA Hiroyuki
Resource classification: Experience equipment, Facilities, etc
Main purpose: Research on environmental fatigue strength of an
aerospace structure components
Load range: (±50, ±25. ±10, ±5) ton
Control system: Load, displacement, strain
Test items: Static load test by computer control, Fracture
toughnes test, arbitrary randon fatigue test
Maximum stroke: +-100 mm
Test environment: (1) Temperature -60 to +150 deg.C
Humidity 30 to 95% R.H.
(2) Temperature RT to 350 deg.C
(3) Temperature RT to 1,700 deg.C
Effective distance: 1,200mm
Completion: Fiscal 1987, 1989
User procedures and method:
[Procedure for Use]
Refer in detail to Business Squad, Planning Room.
[Charge for Use]
According to the calculation standard of acceptance research
expenses appointed by the Science and Technology Agency.
[Restriction for use]
Uses by a person not belonging to national administration
organs are limited to a case approved to be especially
necessary for improvement of aeronautical technology and
space technology.

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