Space Use Materials Strength Data Sheet (SDS)
About Space Use Materials Strength Data Sheet (SDS) Online
NIMS structural materials data sheets contain various types of data (e.g., creep, fatigue, corrosion and cryogenic fatigue properties) collected systematically and without bias using standardized testing methods. For more than 40 years, these data sheets have provided industry with fundamental data for determining appropriate design stress and selecting proper materials to enable the design of machines and structures of adequate strength. They have also been used as reference materials to estimate the degree of deterioration and the remaining life of various materials in use.
This site contains "space use materials strength data sheet" among NIMS structural materials data sheets.
※The URL for Space Use Materials Strength Data Sheet (SDS) has changed. (Jan 17, 2023)
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●New URL: https://sds.nims.go.jp/
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E-Mail: datasht=nims.go.jp ( [ = ] → [ @ ] )
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Recorded Data
| Base element | Materials | DS No. | Properties | Testing temp. / K |
|
|---|---|---|---|---|---|
| -- | Data Sheet Program | 0 | -- | -- | |
| Ti | Ti-5Al-2.5Sn ELI Alloy | Φ180Billet | 1 | Tensile | 4, 20, 77, 293 |
| Charpy impact | 4, 77, 293 | ||||
| Fracture toughness | 4, 20, 77, 293 | ||||
| High-cycle fatigue (Uniaxial constant stress) |
|||||
| 14 | Fatigue crack growth rate | 20, 293 | |||
| Φ160Billet | 3 | Tensile | 4, 20, 77, 293 | ||
| Charpy impact | 4, 77, 293 | ||||
| Fracture toughness | 4, 20, 77, 293 | ||||
| High-cycle fatigue (Uniaxial constant stress) |
|||||
| Ti-6Al-4V ELI ALLOY | Φ300Billet | 23 | Tensile | 20, 77, 293 | |
| Fracture toughness | 20, 77, 293 | ||||
| High-cycle fatigue (Uniaxial constant stress) |
|||||
| Ni | Alloy 718 plate (1228K ST) |
Welded joints | 2 | Tensile | 77, 298 |
| Fracture toughness | |||||
| Low-cycle fatigue | 77, 113, 298 | ||||
| Base metal and welded Joints | 20 | Tensile | 77, 293, 873 | ||
| Fracture toughness | |||||
| High-cycle fatigue (Uniaxial constant stress) |
|||||
| AMS5596 | 21 | High-cycle fatigue - Notch Effect- (Uniaxial Constant Stress) |
77, 293, 873 | ||
| AMS5596 | 22 | Fatigue crack growth rate | 77, 293, 873 | ||
| Alloy 718 plate (1318 K ST) | Base metal and welded joints | 4 | Tensile | 77, 113, 293, 873 | |
| Fracture toughness | 77, 293, 873 | ||||
| High-cycle Fatigue (Uniaxial Constant Stress) |
77, 113, 293, 873 | ||||
| 8 | High-cycle fatigue - Notch Effect - (Uniaxial Constant Stress) |
77, 113, 293, 873 | |||
| 9 | Fatigue crack growth rate | 77, 293, 873 | |||
| 24 | Tensile | 20, 77, 293, 873 | |||
| Fracture toughness | 20, 77, 293, 873 | ||||
| High-cycle Fatigue (Uniaxial Constant Stress) |
77, 293, 873 | ||||
| Alloy 718 plate (1338K ST) |
Base metal and welded joints | 25 | Fatigue crack growth rate | 20, 77, 293, 873 | |
| 28 | Tensile | 20, 77, 293, 873 | |||
| Low-cycle fatigue | 77, 293, 873 | ||||
| Alloy 718 forging | 5 | Tensile | 4, 20, 77, 293, 767 | ||
| Charpy impact | 4, 77, 293 | ||||
| Fracture toughness | 4, 20, 77, 293, 767 | ||||
| High-cycle fatigue (Uniaxial Constant Stress) |
|||||
| 15 | Fatigue crack growth rate | 77, 293, 767 | |||
| Alloy 718 investment casting | 10 | Tensile | 4, 20, 77, 293, 767 | ||
| Charpy impact | 4, 77, 293 | ||||
| Fracture toughness | 4, 20, 77, 293, 767 | ||||
| High-cycle fatigue (Uniaxial Constant Stress) |
|||||
| 18 | Fatigue crack growth rate | 20, 77, 293 and 767 | |||
| Alloy 247 Low carbon directioally solidified | 16 | Tensile | 293, 800 | ||
| High-cycle fatigue (Uniaxial Constant Stress) |
|||||
| Alloy 625 plate | Base metal and welded joints | 26 | Tensile | 77, 293, 873 | |
| High-cycle fatigue (Uniaxial constant stress) |
77, 293, 873 | ||||
| 27 | Tensile | 77, 293, 873 | |||
| Low-cycle fatigue | 77, 293, 873 | ||||
| Fe | Alloy A286 forging | 6 | Tensile | 4, 20, 77, 293, 873 | |
| Charpy impact | 4, 77, 293 | ||||
| Fracture toughness | 4, 20, 77, 293 | ||||
| High-cycle fatigue (Uniaxial constant stress) |
4, 20, 77, 293, 873 | ||||
| 304L forging | 7 | Tensile | 4, 20, 77, 293, 773 | ||
| Charpy impact | 4, 77, 293 | ||||
| Fracture toughness | 4, 20, 77, 293 | ||||
| High-cycle fatigue (Uniaxial constant stress) |
4, 20, 77, 293, 773 | ||||
| Co | Alloy 188 bar | 11 | Tensile | 77, 293, 750 | |
| Charpy impact | 77, 293 | ||||
| High-cycle fatigue (Uniaxial constant stress) |
77, 293, 750 | ||||
| Al | A356-T6 casting | 12 | Tensile | 20, 77, 293 | |
| Fracture toughness | |||||
| High-cycle fatigue (Uniaxial constant stress) |
|||||
| 17 | Fatigue crack growth rate | 20, 77, 293 | |||
| Cu | Cu-Cr-Zr forging | 13 | Tensile | 293, 773, 823, 923 | |
| Creep-rupture | 773, 823, 923 | ||||
| Low-cycle fatigue (symmetrical) | 293, 773, 823, 923 | ||||
| Low-cycle fatigue (tension hold) | 773, 823, 923 | ||||
| Low-cycle fatigue (compression hold) | |||||
| 19 | Creep | 773, 823, 923 | |||
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