Designation
| Name |
The value |
| Designation GOST Cyrillic |
015Н18К13М5ТЮ |
| Designation GOST Latin |
015H18K13M5TJu |
| Transliteration |
015N18K13M5TYu |
| By chemical elements |
015Н18Co13Mo5TiAl |
| Name |
The value |
| Designation GOST Cyrillic |
ЭП948 |
| Designation GOST Latin |
EP948 |
| Transliteration |
EhP948 |
| By chemical elements |
- |
| Name |
The value |
| Designation GOST Cyrillic |
ЧС35 |
| Designation GOST Latin |
ChC35 |
| Transliteration |
ChS35 |
| By chemical elements |
ZrС35 |
Description
015Н18К13М5ТЮ steel is used: for the production of parts and housings of rocket engines, parts of aircraft engines.
Note
Maraging steel with higher structural stability in the temperature range from cryogenic to +500 °C.
Standards
| Name |
Code |
Standards |
| Blanks. Of the workpiece. Slabs |
В31 |
TU 14-1-1214-75 |
| Bars and shapes |
В32 |
TU 14-1-3024-80, TU 14-1-2125-77 |
Chemical composition
| Standard |
C |
S |
P |
Mn |
Si |
Ni |
Fe |
Al |
Ti |
Mo |
Zr |
Co |
| TU 14-1-2125-77 |
≤0.015 |
≤0.01 |
≤0.01 |
0.1 |
≤0.1 |
17.5-18.5 |
Rest |
0.05-0.15 |
0.6-0.8 |
4.5-5 |
≤0.02 |
12.5-13.5 |
Fe is the basis.
