IP 468 : 2001
Withdrawn
Withdrawn
DETERMINATION OF THE FREEZING POINT OF AVIATION TURBINE FUELS - AUTOMATIC OPTICAL METHOD
Published date
01-12-2013
Withdrawn date
07-23-2013
Sorry this product is not available in your region.
Defines an automatic procedure for the determination of the freezing point of aviation turbine fuels over the temperature range of -40 degree C to -70 degree C. The results obtained are equivalent to those obtained using the manual test method IP 16, but a small bias of less than 0,5 degree C has been observed.
| DocumentType |
Standard
|
| PublisherName |
Energy Institute (formerly Institute of Petroleum - IP)
|
| Status |
Withdrawn
|
| DEFSTAN 91-87/3(2002) : 2002 | TURBINE FUEL, AVIATION KEROSENE TYPE, CONTAINING FUEL SYSTEM ICING INHIBITOR NATO CODE: F-34 JOINT SERVICE DESIGNATION: AVTUR/FSII |
Summarise
Sorry this product is not available in your region.