1. Introduce
– Ni-Cr-W heat-resistant metal that can be used at temperatures up to about 1100℃
* MO-RE alloy
– High melting point metal and excellent ductility
– Superior fusibility and high temperature strength gives it an advantage over other refractory alloys in aerospace and energy system applications
– Good creep strength, heat resistance, high temperature strength, and plasticity
| Elemenct | Impact |
|---|---|
| Cr | Provides strength, oxidation resistance |
| W | Provides heat resistance, wear resistance, creep strength |
[MO-RE 1 Chemical Composition (%)]
| C | Cr | Ni | Mo | W |
|---|---|---|---|---|
| 0.4~0.6 | 25.0~28.0 | 35.0~38.0 | Max. 0.5 | 1.5~2.5 |
[MO-RE 1 Mechanical Properties]
| Tensile Strength (Mpa) | Yield Strength (Mpa) | Elongation (%) |
|---|---|---|
| Min. 196 | Min. 412 | Min. 6 |
2. Available Form
– Bar, Rod
– Sheet, Plate, Strip
– Wire
– Powder
3. Application & Product
– Aerospace, Chemical
| Application | Product |
|---|---|
| Aerospace | Space reactor core heating tube |
| Chemical | High temperature furnace heater, High temperature thermocouple |
(1) Space reactor core heating tube / (2) High temperature furnace heater / (3) High temperature thermocouple
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