Description
1.1 This test method covers the determination of the flash point of aviation turbine fuel, diesel fuel, kerosine and related products in the temperature range of 40 °C to 135 °C by a small scale closed cup apparatus.
Product Details
- Published:
- 10/01/2016
- Number of Pages:
- 7
- File Size:
- 1 file , 200 KB
- Redline File Size:
- 2 files , 420 KB
